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Deep in the Oxfordshire countryside, | 0:00:02 | 0:00:04 | |
a group of British rocket scientists are making the final checks | 0:00:04 | 0:00:08 | |
before testing an experimental rocket engine. | 0:00:08 | 0:00:11 | |
Consol armed. | 0:00:15 | 0:00:16 | |
Defying all conventional wisdom, | 0:00:19 | 0:00:22 | |
one man has pursued a dream his entire working life. | 0:00:22 | 0:00:25 | |
Lead engineer Alan Bond believes he is now on the threshold | 0:00:27 | 0:00:31 | |
of realising his dream - to build a revolutionary spacecraft | 0:00:31 | 0:00:35 | |
that achieves Earth orbit in a single leap. | 0:00:35 | 0:00:38 | |
Three, two, one... | 0:00:38 | 0:00:41 | |
Into sequence. | 0:00:41 | 0:00:42 | |
If their calculations are correct, | 0:00:44 | 0:00:47 | |
their revolutionary design will herald by new era in space flight. | 0:00:47 | 0:00:53 | |
WHIRRING | 0:00:53 | 0:00:55 | |
This is the story of how a small and talented group | 0:01:11 | 0:01:15 | |
of British engineers overcame personal adversity, | 0:01:15 | 0:01:19 | |
shrugged off government intransigence | 0:01:19 | 0:01:21 | |
and defeated the Official Secrets Act to pursue a dream. | 0:01:21 | 0:01:25 | |
A dream that began in a boy's back garden shed. | 0:01:33 | 0:01:37 | |
ROCK MUSIC PLAYS | 0:01:38 | 0:01:41 | |
It's traditional in Britain that all things start in a shed. | 0:01:58 | 0:02:01 | |
And we've kept up a long tradition on that. | 0:02:03 | 0:02:07 | |
Alan Bond's passion for space travel began at an early age. | 0:02:07 | 0:02:11 | |
The background really starts back in the 1960s. | 0:02:12 | 0:02:15 | |
Going back to my childhood days, I sort of looked at Dan Dare and saw | 0:02:15 | 0:02:20 | |
that Dan Dare was not constrained to messing about on planet Earth, | 0:02:20 | 0:02:24 | |
he had a whole solar system at his disposal. | 0:02:24 | 0:02:26 | |
Since those days, | 0:02:26 | 0:02:28 | |
I've always felt that the human race has got much more ahead of it | 0:02:28 | 0:02:32 | |
than just being confined to the surface of one little messy planet. | 0:02:32 | 0:02:36 | |
As a teenager, I began to build my own rockets and really got to grips | 0:02:37 | 0:02:42 | |
with what the problems were of getting into space. | 0:02:42 | 0:02:46 | |
It very quickly became apparent that rockets were very limited | 0:02:47 | 0:02:51 | |
in what they can actually do. | 0:02:51 | 0:02:52 | |
And from a very, very early stage, | 0:02:54 | 0:02:56 | |
I realised that we weren't going to get Dan Dare | 0:02:56 | 0:03:00 | |
out of the existing sort of rockets, we've got to have something better. | 0:03:00 | 0:03:04 | |
-RUMBLING -This is a new sound. | 0:03:04 | 0:03:07 | |
The sound of a space age. | 0:03:07 | 0:03:09 | |
The sound of the Blue Streak rocket. | 0:03:09 | 0:03:11 | |
Nonetheless, the possibility existed for a long time throughout the 1960s | 0:03:11 | 0:03:15 | |
that if we could just make the rocket engine a little bit better, | 0:03:16 | 0:03:19 | |
a little bit more efficient, we might be able to come up with | 0:03:19 | 0:03:23 | |
an overall vehicle | 0:03:23 | 0:03:24 | |
which did not have to throw chunks of it away to go into orbit. | 0:03:24 | 0:03:29 | |
The idea was out there that we could and should do better. | 0:03:29 | 0:03:32 | |
As it happened, we didn't get very far with that. | 0:03:32 | 0:03:36 | |
All around the world, many people realised that rockets | 0:03:36 | 0:03:39 | |
in the form that we'd got them were just not going to deliver | 0:03:39 | 0:03:42 | |
in the long term the kind of transport technology | 0:03:42 | 0:03:45 | |
we were looking for. | 0:03:45 | 0:03:46 | |
So virtually every space company in the world was trying to do better. | 0:03:46 | 0:03:51 | |
This is where a rather fortuitous sequence of events occurred. | 0:03:52 | 0:03:56 | |
Back in the very early '80s, | 0:03:56 | 0:03:59 | |
we had a meeting that was organised by the French. | 0:03:59 | 0:04:03 | |
The French wanted to come over and tell us their plans for Ariane 5. | 0:04:03 | 0:04:07 | |
They had plans to put a winged mini shuttle on top of it called Hermes. | 0:04:08 | 0:04:14 | |
Alan and I, who'd known one another for a long time, | 0:04:14 | 0:04:17 | |
sat at the back of this meeting | 0:04:17 | 0:04:19 | |
and we said, "This is Dinosaur reinvented, | 0:04:19 | 0:04:22 | |
"the 1950s United States Air Force thing. | 0:04:22 | 0:04:26 | |
"There must be a better way of entry in the 21st century | 0:04:26 | 0:04:29 | |
"than going with this antique technology." | 0:04:29 | 0:04:32 | |
In round about 1984, | 0:04:43 | 0:04:45 | |
I had a meeting with Bob Parkinson | 0:04:45 | 0:04:48 | |
and John Scott-Scott from Rolls-Royce in my office. | 0:04:48 | 0:04:52 | |
Well, the story was that Alan had been working on something quietly. | 0:04:52 | 0:04:57 | |
Nobody was quite sure what it was. | 0:04:57 | 0:04:59 | |
I'd always been interested in pushing propulsion much harder. | 0:05:01 | 0:05:05 | |
Whilst the solar system and trips to the moon represent a serious challenge, | 0:05:05 | 0:05:09 | |
I'd been interested right from my earliest days | 0:05:09 | 0:05:12 | |
in going much further than that | 0:05:12 | 0:05:14 | |
and that drew me into more advanced propulsion, nuclear propulsion. | 0:05:14 | 0:05:17 | |
One of the things that came out of those studies is that | 0:05:20 | 0:05:23 | |
if you have a hot nuclear reactor on a rocket | 0:05:23 | 0:05:25 | |
and you have cold liquid hydrogen, | 0:05:25 | 0:05:27 | |
I realised that you could replace the nuclear reactor with hot air at roundabout Mach 5. | 0:05:27 | 0:05:32 | |
And that opened up the prospect of a whole new range of engines | 0:05:32 | 0:05:35 | |
that no-one had considered before. | 0:05:35 | 0:05:37 | |
But then one day he turned up at our house, literally, at home... | 0:05:37 | 0:05:41 | |
And he said, "I want to talk to you | 0:05:42 | 0:05:44 | |
"about a possible new propulsion system | 0:05:44 | 0:05:47 | |
"that could actually sort of completely revolutionise rocketry as we know it." | 0:05:47 | 0:05:53 | |
Alan's visionary thinking had come at the right time. | 0:05:53 | 0:05:57 | |
The world was growing tired of the ever-mounting cost of reaching space. | 0:05:57 | 0:06:00 | |
The world was beginning to suffer | 0:06:02 | 0:06:04 | |
from the cost of launching satellites more and more, | 0:06:04 | 0:06:08 | |
because more and more people wanted to put up small clusters, | 0:06:08 | 0:06:12 | |
communication things, land resources. | 0:06:12 | 0:06:14 | |
All the usual things, which at the moment, and still to this day, | 0:06:14 | 0:06:18 | |
are being launched by totally expendable rockets. | 0:06:18 | 0:06:21 | |
Nothing comes back except bits of wreckage. | 0:06:21 | 0:06:24 | |
To reach orbit, conventional rockets burn tons of hydrogen | 0:06:24 | 0:06:27 | |
and oxygen every second. | 0:06:27 | 0:06:29 | |
But when the fuel is spent, empty tanks and rockets | 0:06:29 | 0:06:32 | |
are simply jettisoned to burn up in the planet's atmosphere. | 0:06:32 | 0:06:36 | |
-MAN ON RADIO: -Booster officer, confirm staging a good solid rocket booster separation. | 0:06:37 | 0:06:42 | |
Shut down. Sierra-D's have shut down. BDM fire. | 0:06:42 | 0:06:45 | |
What took thousands of man hours to make | 0:06:50 | 0:06:53 | |
has a working life measured in seconds. | 0:06:53 | 0:06:56 | |
So, people wanted cheaper launching things | 0:07:01 | 0:07:04 | |
and the only way to make it really cheap | 0:07:04 | 0:07:06 | |
is to make it like an airliner. | 0:07:06 | 0:07:08 | |
So I tinkered together the blue book and passed it to John | 0:07:08 | 0:07:13 | |
to find out what his interest was going to be on it. | 0:07:13 | 0:07:15 | |
It's pages and pages of theory and numbers. We turn to the back. | 0:07:15 | 0:07:19 | |
Here we are, paragraph seven, conclusion. | 0:07:19 | 0:07:21 | |
"The report has outlined a proposal for an air-breathing engine | 0:07:21 | 0:07:26 | |
"which may allow a single-stage-to-orbit | 0:07:26 | 0:07:29 | |
"space transportation system to be realised." | 0:07:29 | 0:07:31 | |
Now, normally if you talk to people about that sort of concept, | 0:07:31 | 0:07:35 | |
they will tell you it can't be done. | 0:07:35 | 0:07:37 | |
I examined all the rocket propellants that were available, including some you wouldn't like to work with. | 0:07:39 | 0:07:46 | |
And you just cannot hack it with rockets. | 0:07:47 | 0:07:50 | |
So you've got to make use of the atmosphere, | 0:07:50 | 0:07:52 | |
same as any other aircraft does. | 0:07:52 | 0:07:54 | |
Alan turned to his old friend Bob Parkinson for help. | 0:07:54 | 0:07:58 | |
Alan rang me up to ask me a question about propellant chemistry | 0:08:00 | 0:08:03 | |
and in the discussion over the phone, we said, | 0:08:03 | 0:08:06 | |
"It sounds like we've been working on parallel lines. | 0:08:06 | 0:08:09 | |
"We ought to have a meeting together." | 0:08:09 | 0:08:11 | |
Bob was thinking more about the actual vehicle side of things | 0:08:11 | 0:08:14 | |
and I was thinking more of the propulsion side of things. | 0:08:14 | 0:08:17 | |
The great thing about Bob is that he'd moved to British Aerospace | 0:08:17 | 0:08:21 | |
and he also, because of his very innovative character, | 0:08:21 | 0:08:25 | |
had the ear of the senior management. | 0:08:25 | 0:08:27 | |
As a consequence, he was able to get the project into British Aerospace. | 0:08:27 | 0:08:31 | |
And out of that came the HOTOL project. | 0:08:31 | 0:08:34 | |
The basic idea was simple enough. | 0:08:39 | 0:08:42 | |
Conventional rockets burn a mixture of liquid oxygen and hydrogen. | 0:08:42 | 0:08:46 | |
Hydrogen is an ideal fuel - it's light | 0:08:46 | 0:08:50 | |
and generates huge amounts of thrust. | 0:08:50 | 0:08:52 | |
In comparison, the oxygen it needs to burn is bulky and very heavy. | 0:08:52 | 0:08:57 | |
But Alan Bond thought he saw a way to cut HOTOL's need to store that oxygen on board. | 0:08:59 | 0:09:04 | |
It was obvious the atmosphere has to play a part in getting us into space. | 0:09:06 | 0:09:10 | |
Bond's breakthrough was the idea that HOTOL could steal oxygen | 0:09:11 | 0:09:16 | |
from the atmosphere. | 0:09:16 | 0:09:17 | |
And the whole idea of this was single-stage-to-orbit. | 0:09:20 | 0:09:23 | |
That was the key bottom line. | 0:09:23 | 0:09:24 | |
Now, to do it, if you look at the amount of work you've got to do | 0:09:24 | 0:09:29 | |
to get into orbit, it says use as much oxygen as you can | 0:09:29 | 0:09:33 | |
from any source except what's on the vehicle. | 0:09:33 | 0:09:36 | |
And so you drive yourself into the area of, | 0:09:36 | 0:09:39 | |
"How far can we go as an air-breathing machine?" | 0:09:39 | 0:09:43 | |
And therefore you lean heavily on gas turbine technology, | 0:09:43 | 0:09:46 | |
which is well-established, | 0:09:46 | 0:09:49 | |
and only use rocket technology when, putting it simply, | 0:09:49 | 0:09:52 | |
you've run out of air. | 0:09:52 | 0:09:54 | |
Together, the three engineers secured funding from the UK government, | 0:09:54 | 0:09:59 | |
British Aerospace and Rolls-Royce. | 0:09:59 | 0:10:01 | |
In those first heady days, | 0:10:05 | 0:10:06 | |
Alan's dream looked as though it was becoming a reality. | 0:10:06 | 0:10:09 | |
Bond's theory worked fine on paper, | 0:10:12 | 0:10:15 | |
but experiments in the lab soon brought disappointment and delay. | 0:10:15 | 0:10:18 | |
There were several problems with HOTOL. | 0:10:22 | 0:10:24 | |
One was the actual design of the aeroplane itself, | 0:10:24 | 0:10:26 | |
which was a magnificent attempt. | 0:10:26 | 0:10:28 | |
The other was the engine. There were issues over the engine. | 0:10:28 | 0:10:33 | |
To reach orbit from sea level, | 0:10:33 | 0:10:35 | |
HOTOL's engines would have to work flawlessly at extreme temperatures. | 0:10:35 | 0:10:40 | |
The air comes in at 1,000 degrees Centigrade as it slows down | 0:10:40 | 0:10:44 | |
and you can't put that through a compressor, | 0:10:44 | 0:10:46 | |
in fact, it's very difficult | 0:10:46 | 0:10:48 | |
to design the airframe to stand it for very long. | 0:10:48 | 0:10:51 | |
The key Alan came up with was to take that air coming in, | 0:10:51 | 0:10:55 | |
accept it in heat-resisting duct for the first little bit | 0:10:55 | 0:10:59 | |
and then cool it - drastically. | 0:10:59 | 0:11:02 | |
Alan's first choice | 0:11:08 | 0:11:10 | |
was to cool this thing right down | 0:11:10 | 0:11:12 | |
to just above the liquefaction point of the air which we breathe. | 0:11:12 | 0:11:17 | |
That's a long way down, but it could be done. | 0:11:17 | 0:11:20 | |
Bond's second breakthrough | 0:11:20 | 0:11:22 | |
was how he planned to cool the air entering HOTOL's rocket engines. | 0:11:22 | 0:11:25 | |
You've got hydrogen on board this vehicle, | 0:11:25 | 0:11:29 | |
which is a wonderful coolant. | 0:11:29 | 0:11:30 | |
By using HOTOL's liquid hydrogen fuel | 0:11:30 | 0:11:33 | |
to cool and compress the incoming air, | 0:11:33 | 0:11:36 | |
HOTOL only had to carry small amounts of oxygen | 0:11:36 | 0:11:39 | |
for when the vehicle reached space, | 0:11:39 | 0:11:41 | |
saving weight that could be used to carry cargo. | 0:11:41 | 0:11:45 | |
What we've got here is a typical experimental heat exchanger | 0:11:48 | 0:11:51 | |
from the HOTOL programme. | 0:11:51 | 0:11:53 | |
The liquid nitrogen went into these tubes at the end, | 0:11:53 | 0:11:57 | |
all the way through these fine tubes and out the other side. | 0:11:57 | 0:12:00 | |
The air flowed through there. | 0:12:00 | 0:12:02 | |
When we looked at the transit time | 0:12:02 | 0:12:05 | |
for air going through the heat exchanger or pre-cooler, | 0:12:05 | 0:12:08 | |
the answer comes out between one and two milliseconds. | 0:12:08 | 0:12:12 | |
That's a pretty short time for all this heat to be removed - bump! | 0:12:12 | 0:12:15 | |
The first experiments we did on rapid cooling | 0:12:18 | 0:12:21 | |
showed us that within literally 4-5 seconds, | 0:12:21 | 0:12:24 | |
the heat exchanger module would frost up solid - | 0:12:24 | 0:12:28 | |
no air flow through it at all. | 0:12:28 | 0:12:30 | |
It highlighted the key problem was not so much heat exchange, | 0:12:30 | 0:12:34 | |
which we believed we could do, | 0:12:34 | 0:12:36 | |
but how do we tackle the frosting problem? | 0:12:36 | 0:12:39 | |
Frost control wasn't the only problem the HOTOL team encountered. | 0:12:41 | 0:12:45 | |
Flaws in the airframe design soon became glaringly obvious. | 0:12:45 | 0:12:49 | |
Richard Varvill, a young aerospace engineer joining the team, | 0:12:50 | 0:12:54 | |
grappled with the spacecraft's aerodynamics. | 0:12:54 | 0:12:57 | |
We'd basically made a mistake right at square one, | 0:12:58 | 0:13:01 | |
which was to put the engines on the base of the fuselage. | 0:13:01 | 0:13:04 | |
You have to go back to the origins of the HOTOL project to understand how this problem came about, | 0:13:04 | 0:13:09 | |
we came from a background of vertical take-off rockets, | 0:13:09 | 0:13:12 | |
where, as you know, the engines are always on the base of the rocket | 0:13:12 | 0:13:14 | |
and it ascends vertically and you have the tankage above it. | 0:13:14 | 0:13:17 | |
On HOTOL, that seemed like a good starting point, | 0:13:17 | 0:13:21 | |
so we ended up with this long, slender hydrogen tank | 0:13:21 | 0:13:24 | |
sticking out ahead of the wings | 0:13:24 | 0:13:26 | |
because it gave a very structurally efficient configuration | 0:13:26 | 0:13:30 | |
for the airframe. | 0:13:30 | 0:13:31 | |
However, what we found was this very severe CGCP mismatch. | 0:13:34 | 0:13:38 | |
When fully fuelled, the weight of the hydrogen | 0:13:40 | 0:13:43 | |
balanced the weight of the engines at the rear of the craft. | 0:13:43 | 0:13:47 | |
But as the fuel was used up in flight, | 0:13:47 | 0:13:49 | |
the centre of gravity of the craft | 0:13:49 | 0:13:51 | |
shifted backwards towards the engines. | 0:13:51 | 0:13:54 | |
The centre of pressure, however, was forced forward, | 0:13:54 | 0:13:56 | |
leading to flight instability. | 0:13:56 | 0:13:59 | |
Or, as aerospace engineers call it, a CGCP mismatch. | 0:13:59 | 0:14:05 | |
To resolve this, we ended up making a lot of undesirable changes | 0:14:05 | 0:14:08 | |
to the aeroplane | 0:14:08 | 0:14:09 | |
and in the process, we lost, we reckon, | 0:14:09 | 0:14:12 | |
about four tonnes of potential payload. | 0:14:12 | 0:14:14 | |
'T-10, 9, 8, 7, 6, 5, 4... | 0:14:14 | 0:14:21 | |
'We've gone for main engine start. We have main engine start.' | 0:14:21 | 0:14:24 | |
From the outset, Britain had designed HOTOL | 0:14:24 | 0:14:26 | |
as a replacement for NASA's space shuttle. | 0:14:26 | 0:14:29 | |
'America's first space shuttle. | 0:14:31 | 0:14:32 | |
'And the shuttle has cleared the tower.' | 0:14:32 | 0:14:35 | |
Colombia had successfully launched a year earlier | 0:14:35 | 0:14:38 | |
with the specific goal of carrying payloads into space. | 0:14:38 | 0:14:42 | |
'We have main-engine start.' | 0:14:42 | 0:14:44 | |
'2, 1, booster ignition. And the final lift-off of Discovery.' | 0:14:45 | 0:14:51 | |
Whereas a space shuttle could carry 22 tonnes of cargo, | 0:14:53 | 0:14:56 | |
HOTOL's design capacity of 8 tonnes had now been reduced by half. | 0:14:56 | 0:15:02 | |
Unlike HOTOL, NASA's shuttle was a two-stage-to-orbit vehicle | 0:15:14 | 0:15:20 | |
with the vast majority of the rocket discarded | 0:15:20 | 0:15:23 | |
within minutes of take-off. | 0:15:23 | 0:15:24 | |
NASA described its space transportation system | 0:15:31 | 0:15:34 | |
as a kind of reusable space truck, | 0:15:34 | 0:15:36 | |
with each vehicle designed for a lifespan of 100 launches. | 0:15:36 | 0:15:40 | |
'3, 2, 1...' | 0:15:42 | 0:15:46 | |
In reality, in the 30 years the programme ran, | 0:15:46 | 0:15:49 | |
only a total of 135 flights were ever made. | 0:15:49 | 0:15:53 | |
But the shuttle remains | 0:16:02 | 0:16:04 | |
the only winged, manned and reusable spacecraft | 0:16:04 | 0:16:07 | |
to have successfully reached orbit and landed again. | 0:16:07 | 0:16:11 | |
'Main gear touchdown.' | 0:16:11 | 0:16:14 | |
'Nose gear touchdown.' | 0:16:26 | 0:16:28 | |
The shuttle programme may not have lived up to its original billing, | 0:16:28 | 0:16:32 | |
but it had the overriding merit that it actually worked. | 0:16:32 | 0:16:36 | |
With all its technical difficulties and its payload capacity halved, | 0:16:36 | 0:16:39 | |
the economic case for HOTOL was now on shaky ground. | 0:16:39 | 0:16:43 | |
We do need to have a look at greater commercial involvement | 0:16:43 | 0:16:46 | |
and consider really exactly what the strategy is | 0:16:46 | 0:16:50 | |
before we go into this highly expensive, | 0:16:50 | 0:16:52 | |
I think, not altogether well-directed space effort. | 0:16:52 | 0:16:55 | |
Despite Alan Bond's best efforts to persuade ministers | 0:16:55 | 0:16:59 | |
of the technical and commercial viability of his project, | 0:16:59 | 0:17:03 | |
they remained unconvinced. | 0:17:03 | 0:17:04 | |
The man in the street expects ministers | 0:17:06 | 0:17:09 | |
to evaluate these hugely expensive claims, | 0:17:09 | 0:17:11 | |
and until and unless these enthusiasts, | 0:17:11 | 0:17:15 | |
at home and abroad, satisfy us there's good value for money, | 0:17:15 | 0:17:18 | |
I think it's the duty of ministers to say, | 0:17:18 | 0:17:20 | |
"We admire your enthusiasm, but that bill is simply too much." | 0:17:20 | 0:17:24 | |
With all government funding for HOTOL now gone, | 0:17:25 | 0:17:29 | |
Alan's dream was in tatters. | 0:17:29 | 0:17:31 | |
As a last resort, he sought backing from Europe. | 0:17:31 | 0:17:35 | |
He intended to take his engine design | 0:17:38 | 0:17:41 | |
to the European Space Agency and continue his work there. | 0:17:41 | 0:17:45 | |
But once again, the government stood in his way. | 0:17:46 | 0:17:50 | |
Following meetings between Bob and myself | 0:17:53 | 0:17:55 | |
and some of the other people involved, | 0:17:55 | 0:17:57 | |
it was agreed that I would apply for a patent on the RB545 engine. | 0:17:57 | 0:18:03 | |
That immediately brought a classification. | 0:18:04 | 0:18:07 | |
That was a disaster to the HOTOL project. | 0:18:11 | 0:18:14 | |
It meant that we couldn't talk to the European Space Agency | 0:18:16 | 0:18:19 | |
and we were never able to disclose at the time to the European Space Agency | 0:18:19 | 0:18:23 | |
how this engine worked and what the advances in it were. | 0:18:23 | 0:18:26 | |
When the thing was classified "secret," | 0:18:26 | 0:18:30 | |
it immediately brings it to "military use only." | 0:18:30 | 0:18:33 | |
That meant that I couldn't talk to anyone about it, | 0:18:33 | 0:18:37 | |
and even got leaned on not to talk to anyone in the UK about it, | 0:18:37 | 0:18:41 | |
including people at Rolls-Royce and British Aerospace. | 0:18:41 | 0:18:44 | |
I had to fight that, otherwise there would have been no project. | 0:18:44 | 0:18:47 | |
I was successful, but for the period up till 1993, | 0:18:47 | 0:18:50 | |
many years after the project had actually finished, | 0:18:50 | 0:18:53 | |
the engine remained classified. | 0:18:53 | 0:18:55 | |
In pursuit of his boyhood dream, Alan had started his career | 0:18:57 | 0:19:01 | |
working on Britain's first attempt to put a payload into space. | 0:19:01 | 0:19:04 | |
On 28th October 1971, | 0:19:06 | 0:19:08 | |
Black Arrow successfully placed into orbit Prospero, | 0:19:08 | 0:19:11 | |
an experimental satellite designed to test | 0:19:11 | 0:19:15 | |
the effects of space on communication satellites. | 0:19:15 | 0:19:19 | |
Ironically, the Black Arrow programme had already been cancelled | 0:19:23 | 0:19:27 | |
three months earlier by the government, on economic grounds. | 0:19:27 | 0:19:31 | |
To this day, Prospero remains the only British satellite | 0:19:32 | 0:19:37 | |
to have been launched by a British-built rocket. | 0:19:37 | 0:19:40 | |
For Alan, this was the start of a long and difficult relationship | 0:19:42 | 0:19:47 | |
with government funding for UK space projects. | 0:19:47 | 0:19:49 | |
That is a problem in Britain. Britain these days is not visionary. | 0:19:51 | 0:19:56 | |
There is a world out there. | 0:19:56 | 0:19:58 | |
The earth is a very, very tiny place in our universe, | 0:19:58 | 0:20:01 | |
and I think you need a certain amount of scientific knowledge | 0:20:01 | 0:20:05 | |
to appreciate that, and I think, by and large in Britain, | 0:20:05 | 0:20:08 | |
scientific knowledge is now rather a limited commodity. | 0:20:08 | 0:20:10 | |
Britain had closed the door on an active role in space vehicles, | 0:20:12 | 0:20:17 | |
and with it, independent access to space. | 0:20:17 | 0:20:20 | |
In America, however, | 0:20:27 | 0:20:29 | |
NASA was still pursuing the concept of a single-stage-to-orbit vehicle. | 0:20:29 | 0:20:33 | |
In 1986, as HOTOL was still underway, | 0:20:34 | 0:20:37 | |
President Reagan had announced | 0:20:37 | 0:20:40 | |
the United States' National Aerospace Program. | 0:20:40 | 0:20:43 | |
But rather than looking at | 0:20:50 | 0:20:52 | |
exotic and unproven engine designs like Alan Bond, | 0:20:52 | 0:20:55 | |
NASA wanted to build on the relative success of its Shuttle program. | 0:20:55 | 0:20:59 | |
It was firmly convinced that rockets were still capable | 0:21:03 | 0:21:06 | |
of propelling a spacecraft to orbit in a single stage. | 0:21:06 | 0:21:09 | |
Even as the United Kingdom was cancelling HOTOL in 1989, | 0:21:13 | 0:21:19 | |
in America, the government commissioned | 0:21:19 | 0:21:21 | |
a series of technology demonstrators for a single-stage-to-orbit vehicle. | 0:21:21 | 0:21:25 | |
Whilst in the UK, Alan struggled to find backers | 0:21:29 | 0:21:32 | |
for a successor to the HOTOL project, | 0:21:32 | 0:21:34 | |
in the US, Lockheed Martin was building the X-33 prototype. | 0:21:34 | 0:21:39 | |
The X-33 was never completed before it too was cancelled. | 0:21:44 | 0:21:47 | |
But in stark contrast to the position of the British government, | 0:21:47 | 0:21:52 | |
the United States continued to pursue its goal | 0:21:52 | 0:21:54 | |
of a reusable single-stage-to-orbit vehicle. | 0:21:54 | 0:21:58 | |
Back in the UK, | 0:22:15 | 0:22:16 | |
in frustration at the government's unwillingness to fund | 0:22:16 | 0:22:20 | |
or even permit a successor to the HOTOL project, | 0:22:20 | 0:22:23 | |
Alan and two of his colleagues, | 0:22:23 | 0:22:25 | |
Richard Varvill and John Scott-Scott, decided to go it alone. | 0:22:25 | 0:22:29 | |
They formed a new company, Reaction Engines, to continue development. | 0:22:30 | 0:22:34 | |
The fledgling company was based in Culham near Oxford, | 0:22:37 | 0:22:42 | |
on the same site as the Joint European Torus | 0:22:42 | 0:22:44 | |
where Alan had worked before transferring to the HOTOL project. | 0:22:44 | 0:22:48 | |
The Joint European Torus is a research reactor | 0:22:51 | 0:22:54 | |
designed to harness the power of nuclear fusion, | 0:22:54 | 0:22:59 | |
the same energy that powers the sun. | 0:22:59 | 0:23:02 | |
In such an environment, they rely heavily | 0:23:03 | 0:23:06 | |
on computer modelling techniques | 0:23:06 | 0:23:08 | |
to predict the behaviour of their experiments | 0:23:08 | 0:23:10 | |
before trying them out for real. | 0:23:10 | 0:23:13 | |
You could do an awful lot of modelling. | 0:23:13 | 0:23:16 | |
You'd think that the aerospace business was the place | 0:23:16 | 0:23:19 | |
that you'd learn that, but back in the 1970s, | 0:23:19 | 0:23:22 | |
computers weren't very available. | 0:23:22 | 0:23:24 | |
It took a long time to get onto a mainframe. | 0:23:24 | 0:23:26 | |
Also, the actual analytical techniques that were used | 0:23:28 | 0:23:31 | |
in the aerospace business at that time were very limited, | 0:23:31 | 0:23:34 | |
so you tended to make things and break them, | 0:23:34 | 0:23:37 | |
and make 'em and break 'em until they worked, | 0:23:37 | 0:23:40 | |
whereas the Atomic Energy Authority were building things | 0:23:40 | 0:23:43 | |
that, if you broke them, were actually quite dangerous, | 0:23:43 | 0:23:46 | |
so they had come up with a great deal more modelling | 0:23:46 | 0:23:49 | |
than the aerospace industry had. | 0:23:49 | 0:23:52 | |
I was fortunate that when I came to Culham to work on fusion, | 0:23:57 | 0:24:01 | |
I learned a lot about that, and I was able to apply that, | 0:24:01 | 0:24:05 | |
so given, suddenly, a PC of my own, | 0:24:05 | 0:24:07 | |
I found that I was already on my old Spectrum able to do an awful lot | 0:24:07 | 0:24:13 | |
that was still being carried out, say, in British Aerospace. | 0:24:13 | 0:24:16 | |
Using the techniques he had learned at JET, | 0:24:16 | 0:24:18 | |
Alan was able to continue working on HOTOL's legacy | 0:24:18 | 0:24:22 | |
without so much as a penny of government funding. | 0:24:22 | 0:24:25 | |
When we finished with the HOTOL project, | 0:24:33 | 0:24:36 | |
there were a number of outstanding issues. | 0:24:36 | 0:24:40 | |
The computer modelling, sort of using ideal conditions, | 0:24:40 | 0:24:44 | |
showed that there was tremendous actual potential behind the concept. | 0:24:44 | 0:24:47 | |
But what we actually found | 0:24:47 | 0:24:49 | |
when we'd come to wrapping all the metallic materials around it | 0:24:49 | 0:24:52 | |
and the ceramics and so on, is a lot of that disappeared | 0:24:52 | 0:24:55 | |
for all kinds of reasons, and for the first three or four years, | 0:24:55 | 0:24:59 | |
the activity was simply to try and find out why we had done so badly | 0:24:59 | 0:25:03 | |
with real engineering relative to the ideal. | 0:25:03 | 0:25:06 | |
And that was down to the actual configuration of the aeroplane. | 0:25:06 | 0:25:09 | |
We resolved that very quickly. | 0:25:09 | 0:25:11 | |
Computer modelling allowed the team to question every assumption | 0:25:13 | 0:25:17 | |
behind HOTOL's configuration, | 0:25:17 | 0:25:19 | |
and redesign it from the ground up. | 0:25:19 | 0:25:21 | |
We decided to literally start with a clean sheet of paper. | 0:25:22 | 0:25:25 | |
And the way we did that was, | 0:25:25 | 0:25:27 | |
we took the engines off the base of the aeroplane, | 0:25:27 | 0:25:31 | |
and we put them actually onto the wing tips. | 0:25:31 | 0:25:34 | |
With one bound, Jack was free | 0:25:35 | 0:25:38 | |
and we got a very efficient solution to that problem. | 0:25:38 | 0:25:40 | |
The solution was a complete overhaul of the airframe. | 0:25:40 | 0:25:44 | |
The new craft was named Skylon. | 0:25:44 | 0:25:48 | |
Although they had designed it, | 0:25:49 | 0:25:51 | |
Bond's new company, Reaction Engines, would not build the plane, | 0:25:51 | 0:25:55 | |
but develop the engines that would allow Skylon to fly. | 0:25:55 | 0:25:59 | |
Whilst Bond continued to work | 0:26:10 | 0:26:11 | |
on developing the original HOTOL concept, NASA changed tack. | 0:26:11 | 0:26:17 | |
It abandoned rocket technology altogether. | 0:26:17 | 0:26:23 | |
Instead, it turned to a development of jet-engine technology, | 0:26:23 | 0:26:27 | |
called scramjet. | 0:26:27 | 0:26:30 | |
Scramjets work much like a modern airliner, | 0:26:40 | 0:26:44 | |
but use their own speed to compress air into their jet engines. | 0:26:44 | 0:26:49 | |
Scramjets are air-breathers, | 0:26:49 | 0:26:51 | |
that obtain oxygen from the air in which it's flying. | 0:26:51 | 0:26:54 | |
This characteristic allows for much more aeroplane-like operations, | 0:26:54 | 0:26:58 | |
with increased safety, affordability and flexibility. | 0:26:58 | 0:27:02 | |
Scramjets are beautifully simple. | 0:27:07 | 0:27:10 | |
They have no moving parts. | 0:27:10 | 0:27:12 | |
A conventional jet has a series of blades | 0:27:13 | 0:27:17 | |
to compress air into the engine. | 0:27:17 | 0:27:20 | |
In a scramjet, however, there are no blades. | 0:27:20 | 0:27:23 | |
The incoming air is compressed by the craft's sheer speed alone. | 0:27:23 | 0:27:28 | |
But as engineers found, igniting fuel at Mach 5 | 0:27:29 | 0:27:33 | |
is about as hard as striking a match in a hurricane, | 0:27:33 | 0:27:37 | |
and keeping it lit - harder still. | 0:27:37 | 0:27:39 | |
Nevertheless, NASA was confident that scramjet technology | 0:27:41 | 0:27:44 | |
would shape the future of manned space flight. | 0:27:44 | 0:27:48 | |
The ultimate goal of hypersonics really is twofold. | 0:27:48 | 0:27:51 | |
One is to reduce the cost for access to space. | 0:27:51 | 0:27:56 | |
The second goal, and probably one that's further out, | 0:27:56 | 0:28:00 | |
maybe 100 years out, | 0:28:00 | 0:28:01 | |
but hypersonic commercial travel, I think, can be a reality someday, | 0:28:01 | 0:28:06 | |
and going anywhere on the globe in just a few hours. | 0:28:06 | 0:28:10 | |
Actuator on my mark. | 0:28:10 | 0:28:13 | |
Three, two, one, mark. | 0:28:13 | 0:28:15 | |
In 2004, NASA's X43 technology demonstrator | 0:28:18 | 0:28:22 | |
set a new airspeed record for powered flight, | 0:28:22 | 0:28:26 | |
reaching an incredible Mach 9.8. | 0:28:26 | 0:28:29 | |
But scramjets can only function at velocities greater than Mach 4 | 0:28:30 | 0:28:35 | |
and must rely on chemical rockets | 0:28:35 | 0:28:37 | |
to boost them up to their operating speed. | 0:28:37 | 0:28:41 | |
As a result, NASA now doubts | 0:28:41 | 0:28:43 | |
that a single-stage-to-orbit spacecraft will ever be achievable. | 0:28:43 | 0:28:47 | |
Console on. | 0:28:54 | 0:28:55 | |
WHIRRING | 0:28:55 | 0:28:58 | |
Just as NASA was announcing the death knell | 0:29:02 | 0:29:05 | |
for single-stage-to-orbit vehicles, | 0:29:05 | 0:29:07 | |
back in the UK, | 0:29:07 | 0:29:08 | |
Bond's team had made a breakthrough in their engine design. | 0:29:08 | 0:29:12 | |
In 2004 we found an entirely new avenue | 0:29:13 | 0:29:16 | |
which we could evolve with these engines. | 0:29:16 | 0:29:20 | |
And the thermodynamics continues to evolve even now, | 0:29:20 | 0:29:23 | |
so we are currently working on an engine | 0:29:23 | 0:29:26 | |
which has half the fuel consumption | 0:29:26 | 0:29:28 | |
of the SABRE engines that we designed in 1993 for the Skylon vehicle, | 0:29:28 | 0:29:33 | |
which in itself was more than 50 per cent improvement | 0:29:33 | 0:29:36 | |
over the engines in HOTOL. | 0:29:36 | 0:29:38 | |
So I don't think we're near the end | 0:29:38 | 0:29:41 | |
of what these engines are actually capable of at this point in time. | 0:29:41 | 0:29:44 | |
To bring the original HOTOL concept to this stage | 0:29:50 | 0:29:53 | |
had taken Alan's team some 15 years. | 0:29:53 | 0:29:56 | |
Along the way, they'd had to overcome a series of obstacles, | 0:29:56 | 0:29:59 | |
which might easily have broken a lesser man. | 0:29:59 | 0:30:02 | |
When Alan first formed Reaction Engines to develop HOTOL's legacy, | 0:30:05 | 0:30:09 | |
the engine he had designed had been classified Top Secret, | 0:30:09 | 0:30:13 | |
and its key features patented. | 0:30:13 | 0:30:16 | |
The actual patent restriction ended in 1993. | 0:30:16 | 0:30:19 | |
The patent had actually been acquired by Rolls-Royce, | 0:30:22 | 0:30:25 | |
for a finite period of time, and it was quite clear | 0:30:25 | 0:30:28 | |
that no further development was going to take place on that engine. | 0:30:28 | 0:30:31 | |
So I set out to find a way to circumvent the patent | 0:30:33 | 0:30:37 | |
in order that we could actually complete the work on it. | 0:30:37 | 0:30:41 | |
Now, I wrote the original patent, so I'd written it in a way | 0:30:41 | 0:30:44 | |
that I didn't think it could be circumvented. | 0:30:44 | 0:30:47 | |
But what we had found during the course of the work | 0:30:50 | 0:30:53 | |
were a lot of thermodynamic nuances within the engine. | 0:30:53 | 0:30:57 | |
And that meant that the engines were capable of things | 0:30:57 | 0:31:00 | |
that in the 1980s I hadn't actually realised. | 0:31:00 | 0:31:04 | |
Having overcome the legal obstacles, | 0:31:06 | 0:31:09 | |
the team now faced a series of daunting technical challenges. | 0:31:09 | 0:31:12 | |
We need the thrust-to-weight ratio of a rocket engine, | 0:31:12 | 0:31:15 | |
but we need the fuel consumption of a jet engine. | 0:31:15 | 0:31:18 | |
So we're basically trying to stitch these two technologies together, | 0:31:18 | 0:31:21 | |
but in order to do that | 0:31:21 | 0:31:23 | |
we need to develop these lightweight heat exchangers. | 0:31:23 | 0:31:26 | |
The key to Skylon's revolutionary engine is its ability, | 0:31:29 | 0:31:33 | |
like a jet engine, to compress incoming air. | 0:31:33 | 0:31:36 | |
Then, like a rocket engine, | 0:31:36 | 0:31:38 | |
to use that air to burn the on-board liquid hydrogen to create thrust. | 0:31:38 | 0:31:44 | |
To do that, the compressed air must first be cooled | 0:31:46 | 0:31:49 | |
until it nearly liquefies. | 0:31:49 | 0:31:51 | |
And that's the bit that no-one has ever successfully done before. | 0:31:51 | 0:31:57 | |
The SABRE engine... | 0:31:57 | 0:31:59 | |
is effectively a jet engine and a rocket engine stitched together. | 0:31:59 | 0:32:04 | |
In order to make this work, | 0:32:04 | 0:32:06 | |
we need these very high-performance heat exchangers. | 0:32:06 | 0:32:09 | |
It is the heat exchangers | 0:32:09 | 0:32:11 | |
that make a single-stage-to-orbit vehicle possible. | 0:32:11 | 0:32:15 | |
Nobody's ever made this type of product before. | 0:32:15 | 0:32:17 | |
No-one's been able to make this type of product before. | 0:32:17 | 0:32:22 | |
The heat exchanger works a bit like a conventional fridge. | 0:32:26 | 0:32:29 | |
Liquid helium is passed through a series of very fine tubes. | 0:32:29 | 0:32:34 | |
Air passing over the tubes is then instantly cooled. | 0:32:34 | 0:32:39 | |
The problem Alan and his team faced | 0:32:39 | 0:32:41 | |
was to manufacture a heat exchanger with as many tubes as possible. | 0:32:41 | 0:32:46 | |
You can't just bend these tubes into any old shape. | 0:32:46 | 0:32:49 | |
They're very unique items, they're unique to Reaction Engines, | 0:32:49 | 0:32:52 | |
we've developed the manufacturing processes in order to build them. | 0:32:52 | 0:32:57 | |
If you take one of these tubes in your hands | 0:32:57 | 0:32:59 | |
you can very easily just break it in two. | 0:32:59 | 0:33:01 | |
So actually forming them into the shapes we need | 0:33:01 | 0:33:05 | |
is a very difficult challenge. | 0:33:05 | 0:33:06 | |
The air is a very poor conductor of heat, | 0:33:11 | 0:33:13 | |
so we have to do everything we can to strive for maximum compactness, | 0:33:13 | 0:33:17 | |
to maximise the heat-transfer performance | 0:33:17 | 0:33:19 | |
on the air side of the heat exchanger, | 0:33:19 | 0:33:21 | |
so a large quantity of these tubular-flow channels | 0:33:21 | 0:33:24 | |
of very small diameter | 0:33:24 | 0:33:27 | |
improves the heat-transfer performance. | 0:33:27 | 0:33:30 | |
Now, we've reached a practical limit | 0:33:30 | 0:33:32 | |
on the compactness that we can achieve. | 0:33:32 | 0:33:34 | |
That's where Reaction Engines is pushing the boundaries | 0:33:34 | 0:33:37 | |
on compact, lightweight heat exchangers. | 0:33:37 | 0:33:41 | |
The challenge here is to cool the air | 0:33:41 | 0:33:43 | |
whilst avoiding the frosting problem | 0:33:43 | 0:33:45 | |
that had bedevilled the original HOTOL project. | 0:33:45 | 0:33:49 | |
It took the team years of research to develop a solution. | 0:33:50 | 0:33:54 | |
But after their disastrous experience with Alan's HOTOL patent, | 0:33:54 | 0:33:58 | |
the team has chosen to keep their latest technology as a trade secret. | 0:33:58 | 0:34:03 | |
We've had a long research programme developing the technology | 0:34:05 | 0:34:08 | |
to stop this pre-cooler clogging up with frost, | 0:34:08 | 0:34:12 | |
and that is unique technology to Reaction Engines. | 0:34:12 | 0:34:15 | |
Trade secrets are how most industries survive. | 0:34:15 | 0:34:19 | |
We have a number of key technologies | 0:34:19 | 0:34:21 | |
and rather than patent those, which basically declares it to the world | 0:34:21 | 0:34:25 | |
how you've done it, what we do is | 0:34:25 | 0:34:28 | |
we basically keep those secrets as trade secrets | 0:34:28 | 0:34:31 | |
within Reaction Engines | 0:34:31 | 0:34:32 | |
and only Reaction Engines' employees are familiar with that knowledge. | 0:34:32 | 0:34:37 | |
The last major technical challenge facing Bond and his team | 0:34:39 | 0:34:42 | |
was getting as much thrust as possible from Skylon's engines, | 0:34:42 | 0:34:46 | |
all the way from the runway, right up to Earth orbit. | 0:34:46 | 0:34:49 | |
Teaming up with Bristol University and Airborne Engineering, | 0:34:53 | 0:34:57 | |
they're exploring techniques called altitude compensation | 0:34:57 | 0:35:00 | |
to make their rocket nozzles ultra-efficient. | 0:35:00 | 0:35:03 | |
Once upon a time you could have a small nozzle for sea level, | 0:35:03 | 0:35:06 | |
throw that away at the end of the first stage | 0:35:06 | 0:35:08 | |
and then have a bigger nozzle in the second stage, | 0:35:08 | 0:35:10 | |
which suits higher altitude - throw that away, | 0:35:10 | 0:35:12 | |
And on the third stage, have the biggest one that you can fit. | 0:35:12 | 0:35:15 | |
So, the advantages that are gained by this altitude compensation | 0:35:15 | 0:35:19 | |
are much more for a single stage, where you can't throw anything away. | 0:35:19 | 0:35:22 | |
All rocket engines work by pushing hot gases through a nozzle | 0:35:34 | 0:35:37 | |
to create the thrust needed to keep the rocket going. | 0:35:37 | 0:35:40 | |
But as the rocket gets higher and higher, | 0:35:43 | 0:35:45 | |
the size of the nozzle needs to get wider and wider | 0:35:45 | 0:35:48 | |
to maintain maximum efficiency. | 0:35:48 | 0:35:50 | |
Unlike the space shuttle, a single-stage-to-orbit vehicle | 0:35:53 | 0:35:56 | |
does not have the luxury of throwing away nozzles | 0:35:56 | 0:35:59 | |
with each booster stage, | 0:35:59 | 0:36:01 | |
so that the right-sized nozzle is always used at any given altitude. | 0:36:01 | 0:36:05 | |
The University of Bristol, to try and get round this problem, | 0:36:12 | 0:36:15 | |
focuses on something called an expansion deflection nozzle. | 0:36:15 | 0:36:18 | |
The idea is fairly simple, | 0:36:18 | 0:36:19 | |
it's a fairly standard shape for the outer contour, | 0:36:19 | 0:36:23 | |
but there's a plug up the middle | 0:36:23 | 0:36:25 | |
which goes up the centre of the engine | 0:36:25 | 0:36:27 | |
and causes a central void in the flow. | 0:36:27 | 0:36:30 | |
As you get higher, it allows the flow to expand in towards the centre line | 0:36:32 | 0:36:36 | |
so you end up with a more efficient engine. | 0:36:36 | 0:36:39 | |
-Just about to do a firing. All ready? -Yes. | 0:36:39 | 0:36:42 | |
BEEPING | 0:36:43 | 0:36:46 | |
What we learned from these tests has been quite interesting. | 0:36:51 | 0:36:55 | |
The rocket engine expansion ratio is bigger than the space shuttle, | 0:36:55 | 0:36:59 | |
so the difference between the exit flow and the central flow | 0:36:59 | 0:37:01 | |
is greater than the space shuttle. | 0:37:01 | 0:37:03 | |
We ran that attached at 12 bar. | 0:37:03 | 0:37:05 | |
The Space Shuttle needs to run at 200 bar to keep it attached. | 0:37:05 | 0:37:09 | |
So we have managed to achieve some fairly impressive results. | 0:37:09 | 0:37:12 | |
Having reached space, | 0:37:24 | 0:37:26 | |
Skylon then faces the equally daunting task of returning again. | 0:37:26 | 0:37:30 | |
The Shuttle famously depended on thousands of ceramic tiles | 0:37:30 | 0:37:34 | |
to protect it from the intense heat caused by re-entry. | 0:37:34 | 0:37:37 | |
The rocketeers needed a lighter-weight solution. | 0:37:39 | 0:37:42 | |
They took their inspiration from an unlikely source - | 0:37:44 | 0:37:47 | |
an American spy plane. | 0:37:47 | 0:37:50 | |
It is drawn from the SR-71 Blackbird, | 0:37:50 | 0:37:52 | |
which had a corrugated titanium skin. | 0:37:52 | 0:37:55 | |
And when we started to look into the Skylon structure, | 0:37:55 | 0:37:58 | |
we decided that the solution that other companies had intended to advocate | 0:37:58 | 0:38:03 | |
which is using honeycomb panels of heat-resisting ceramic material, | 0:38:03 | 0:38:08 | |
was actually not the right way to do it. | 0:38:08 | 0:38:10 | |
And we could find a lighter solution | 0:38:16 | 0:38:19 | |
by adopting the solution that the Blackbird had used, | 0:38:19 | 0:38:23 | |
whereby we just take a single skin of material, | 0:38:23 | 0:38:27 | |
and corrugate it for stiffness, | 0:38:27 | 0:38:29 | |
but also for thermal compliance | 0:38:29 | 0:38:31 | |
from the substructure from which it's mounted. | 0:38:31 | 0:38:33 | |
During re-entry, the aeroshell is about 800 degrees hotter | 0:38:37 | 0:38:41 | |
than the internal structure of the vehicle, | 0:38:41 | 0:38:43 | |
so you've got a major thermal expansion mismatch there to solve. | 0:38:43 | 0:38:47 | |
If you imagine this is part of the aircraft's skin, | 0:38:49 | 0:38:51 | |
it could be part of the fuselage or the wing, | 0:38:51 | 0:38:53 | |
because of the corrugations, | 0:38:53 | 0:38:54 | |
it has a certain amount of stiffness in this direction. | 0:38:54 | 0:38:57 | |
However, it has relatively little stiffness in this direction, | 0:38:57 | 0:39:01 | |
so this panel, during re-entry, could be perhaps 800 degrees hotter | 0:39:01 | 0:39:04 | |
than the substructure from which it's mounted. | 0:39:04 | 0:39:07 | |
It's silicon carbide fibres within a glass matrix. | 0:39:07 | 0:39:11 | |
And this material is good to around 1000 degrees C, we think. | 0:39:11 | 0:39:15 | |
May I have your attention, please? | 0:39:15 | 0:39:17 | |
A temperature run is about to commence. | 0:39:17 | 0:39:20 | |
While Alan's team was drawing on American technology for heat shields, | 0:39:20 | 0:39:25 | |
the United States Air Force had continued to develop the scramjet. | 0:39:25 | 0:39:29 | |
What we are going to do is we are going to take the X-51 Waverider. | 0:39:29 | 0:39:32 | |
We're going to launch that from a B52 at 50,000 feet | 0:39:32 | 0:39:36 | |
over the Pacific Ocean. | 0:39:36 | 0:39:38 | |
And then the vehicle is going to drop away, | 0:39:38 | 0:39:41 | |
it's going to be accelerated by a solid rocket booster up to about Mach 4.5. | 0:39:41 | 0:39:45 | |
The solid rocket booster will drop away and the vehicle, | 0:39:47 | 0:39:50 | |
and the engine, that's just being tested, | 0:39:50 | 0:39:52 | |
is going to ignite and then further accelerate that vehicle up to Mach 6. | 0:39:52 | 0:39:56 | |
The Waverider is the successor to NASA's X-43 scramjet. | 0:39:56 | 0:40:02 | |
But it is designed for conducting warfare, not space travel. | 0:40:02 | 0:40:07 | |
Everything we do at Edwards is flight test | 0:40:07 | 0:40:10 | |
and a lot of what we do is weapon systems - | 0:40:10 | 0:40:12 | |
in the short to middle term - | 0:40:12 | 0:40:14 | |
helping the war fighter more directly. | 0:40:14 | 0:40:17 | |
This is more of a long-term thing. | 0:40:17 | 0:40:18 | |
Things that we're working on in the scramjet engine | 0:40:18 | 0:40:21 | |
are going to benefit the war fighter 15, 20 years from now | 0:40:21 | 0:40:25 | |
when we're will be able to utilise this technology to bring new capabilities to the fight. | 0:40:25 | 0:40:30 | |
It's exciting, though. | 0:40:30 | 0:40:32 | |
NASA had hoped that scramjets would deliver cheap access to space. | 0:40:35 | 0:40:38 | |
But the US Air Force sees scramjets as forming spearhead of prompt global strike - | 0:40:38 | 0:40:45 | |
a military doctrine adopted by the US as part of the war on terror. | 0:40:45 | 0:40:51 | |
Space travel is no longer a goal. | 0:40:51 | 0:40:53 | |
As a means of getting a warhead to any target on the face of the planet in under 15 minutes, | 0:41:00 | 0:41:05 | |
scramjets' disadvantages are of little relevance to the US Air Force. | 0:41:05 | 0:41:09 | |
With scramjet technology firmly focused on military use, | 0:41:15 | 0:41:19 | |
the Skylon team are confident that their own engine design | 0:41:19 | 0:41:22 | |
will now emerge as the sole contender in the race | 0:41:22 | 0:41:26 | |
to produce a single-stage-to-orbit spacecraft. | 0:41:26 | 0:41:29 | |
Our other main competitor in propulsion terms is | 0:41:29 | 0:41:32 | |
the so-called scramjet, supersonic combustion ramjet. | 0:41:32 | 0:41:35 | |
On paper, the scramjet has a sort of siren-like attraction about it, | 0:41:37 | 0:41:42 | |
because it's capable, in theory, of producing useful thrust, | 0:41:42 | 0:41:46 | |
up to some very high Mach numbers. | 0:41:46 | 0:41:48 | |
Perhaps Mach 10 or even 15, on paper. | 0:41:48 | 0:41:52 | |
However, unfortunately, scramjets are completely unsuitable | 0:41:52 | 0:41:56 | |
for propelling an aeroplane into space. | 0:41:56 | 0:41:58 | |
A scramjet, like a ramjet, has no compressor. | 0:42:00 | 0:42:03 | |
So it's not capable of operating from rest. | 0:42:03 | 0:42:05 | |
It has to be accelerated up to some suitable Mach number | 0:42:05 | 0:42:09 | |
before the engine can even generate any thrust whatsoever. | 0:42:09 | 0:42:12 | |
With all the enabling technologies that would turn Skylon into a viable spacecraft now established, | 0:42:21 | 0:42:27 | |
the three rocketeers' lonely years in the wilderness are at last coming to an end. | 0:42:27 | 0:42:33 | |
The journey has been long and arduous. | 0:42:35 | 0:42:38 | |
My overriding feeling is just a sheer waste of time and effort | 0:42:39 | 0:42:43 | |
that's gone into this. | 0:42:43 | 0:42:45 | |
I'm now in my mid-60s. | 0:42:45 | 0:42:47 | |
I really wish I was in my mid-40s, trying to do the same things. | 0:42:47 | 0:42:51 | |
My colleagues have spent a large part of their career | 0:42:52 | 0:42:56 | |
in the wilderness. | 0:42:56 | 0:42:57 | |
We could have done so much more. | 0:42:57 | 0:42:59 | |
You have to remember that originally | 0:42:59 | 0:43:02 | |
HOTOL would have been going to orbit in the mid-1990s | 0:43:02 | 0:43:06 | |
and here we are at least 10 years on from that. | 0:43:06 | 0:43:09 | |
So sad that it's taken us so long and there's been so much wasted time, | 0:43:09 | 0:43:13 | |
especially so much wasted British industry in the process. | 0:43:13 | 0:43:17 | |
From his early work on HOTOL to the present day, | 0:43:19 | 0:43:22 | |
it has taken Bond and his team over 30 years to turn his vision of cheap access to space | 0:43:22 | 0:43:28 | |
into something a lot closer to reality. | 0:43:28 | 0:43:31 | |
There have been many dark days and the real dark days | 0:43:32 | 0:43:35 | |
is when you carry a vision into sort of various government departments | 0:43:35 | 0:43:40 | |
and you feel that people can't see past the first paragraph | 0:43:40 | 0:43:43 | |
of that vision. | 0:43:43 | 0:43:45 | |
But today, vision seems to focus on bank accounts and material wealth | 0:43:45 | 0:43:50 | |
and various celebrity programmes and so on. | 0:43:50 | 0:43:55 | |
The actual vision of doing something bigger | 0:43:55 | 0:43:58 | |
on the basis that the future depends on it seems to have been generally lost. | 0:43:58 | 0:44:02 | |
At an age when many people would be looking forward to retirement, | 0:44:03 | 0:44:07 | |
Alan continues to pursue his dream with passion and determination. | 0:44:07 | 0:44:12 | |
A lot of people have regarded me as having the vision. | 0:44:12 | 0:44:15 | |
I've been fortunate that I've had a large number of colleagues around me | 0:44:17 | 0:44:20 | |
who've also been able to share that vision. | 0:44:20 | 0:44:24 | |
The potential that this technology can add to the science of propulsion | 0:44:24 | 0:44:28 | |
is phenomenal. | 0:44:28 | 0:44:30 | |
Inspired from his boyhood days by the Dan Dare stories, | 0:44:48 | 0:44:51 | |
Alan Bond has devoted his entire life to the dream | 0:44:51 | 0:44:56 | |
of getting mankind into space. | 0:44:56 | 0:44:58 | |
Shrugging off government obduracy, | 0:45:06 | 0:45:09 | |
lack of funding and international scepticism, | 0:45:09 | 0:45:12 | |
he and his colleagues have struggled on against all odds. | 0:45:12 | 0:45:15 | |
Now, more than two decades after the HOTOL Project was shut down, | 0:45:18 | 0:45:23 | |
today's test will decide whether the pre-cooler actually works. | 0:45:23 | 0:45:27 | |
And, with it, the possibility of building an engine | 0:45:28 | 0:45:32 | |
that would allow Skylon to fly. | 0:45:32 | 0:45:34 | |
ENGINE PICKS UP SPEED AND ROARS | 0:45:34 | 0:45:36 | |
The very future of reaction engines itself | 0:45:42 | 0:45:45 | |
depends on the outcome of this test. | 0:45:45 | 0:45:48 | |
The years of hard work pay off. | 0:45:54 | 0:45:58 | |
The pre-cooler works flawlessly. | 0:45:58 | 0:46:00 | |
Alan's vision is finally taking shape. | 0:46:04 | 0:46:07 | |
As of now, Skylon itself remains just a vision. | 0:46:35 | 0:46:39 | |
So far, no-one has come forward to actually build the first prototype. | 0:46:39 | 0:46:44 | |
But such details are of little concern to Alan Bond. | 0:46:45 | 0:46:48 | |
We have absolute confidence in the technology. | 0:46:48 | 0:46:52 | |
I've devoted well over 20 years now into developing this | 0:46:52 | 0:46:55 | |
for the sole reason I'm absolutely sure that it's all going to work. | 0:46:55 | 0:47:00 | |
After a lifetime's devotion to this single dream, | 0:47:00 | 0:47:04 | |
Alan can at last look forward to that dream becoming a reality. | 0:47:04 | 0:47:09 | |
Ten years from now, the first Skylon light vehicles | 0:47:09 | 0:47:13 | |
will be flying into orbit and someone will be looking at the Mark 2. | 0:47:13 | 0:47:17 | |
I like to think of Skylon as the DC3 of the space business. | 0:47:17 | 0:47:21 | |
And somewhere downstream there are the 747s and the 777s. | 0:47:21 | 0:47:26 | |
For the three rocketeers, it has been a lonely journey. | 0:47:27 | 0:47:31 | |
But as Alan approaches his eighth decade stuck on this planet, | 0:47:31 | 0:47:35 | |
at last other people can now see his vision. | 0:47:35 | 0:47:39 | |
There is a new generation of people that do feel | 0:47:39 | 0:47:42 | |
that there's some merit in what we're talking about. | 0:47:42 | 0:47:45 | |
There's a generation of people within government departments in the UK | 0:47:45 | 0:47:50 | |
that feel that there's some merit, | 0:47:50 | 0:47:52 | |
and they have conveyed their views on that to the European Space Agency. | 0:47:52 | 0:47:57 | |
And I do feel that we now are experiencing a seachange | 0:47:57 | 0:48:02 | |
in terms of getting the project moving. | 0:48:02 | 0:48:04 | |
We're standing today, I think, on the verge | 0:48:08 | 0:48:11 | |
of a new era of transportation which will be brought about by these engines, | 0:48:11 | 0:48:16 | |
and I think the possibilities are probably endless. | 0:48:16 | 0:48:20 | |
In a few decades from now, | 0:48:20 | 0:48:22 | |
we'll be able to put anything that we want in space as easily as | 0:48:22 | 0:48:25 | |
we could get on an aeroplane to go anywhere else in the world. | 0:48:25 | 0:48:29 | |
Although I'm slightly visionary, | 0:48:29 | 0:48:31 | |
even I cannot see what the ultimate consequences of all of that are. | 0:48:31 | 0:48:34 | |
Subtitles by Red Bee Media Ltd | 0:48:53 | 0:48:57 |