AHC: Britain be a player in the Space Race

Any missile that's going to be used long term as a deterrent weapon needs to be hypergolic, or better yet solid. Going that route might (possibily) get you a deterrent for a while, but it's a lousy basis for a commercial launcher.
There's nothing wrong with hypergols or solids on a launch vehicle (e.g. Ariane 1-4, Titan, Proton, Dnepr, Scout, all of Delta except the core), plus all of the early Indian and Chinese launchers.
From a modern perspective, most hypergols are fairly nasty and you wouldn't design a launcher today to use them, but anything that's good for an operational missile with a solid service history is a great basis for an early launcher.

No, I'd have them realize that Skybolt isn't the 'thing' sooner, keep the Blue Streak in service longer (say until Polaris subs can take up the deterrent role),
If you want Blue Streak to stand a chance of entering service, you probably have to avoid Skybolt altogether - it was too cheap and credible an alternative (or so it seemed).
Putting Blue Streak into service and then phasing it out in the late '60s has possibilities though, as it might provide surplus missiles and infrastructure.

Get a bit more funding for the Black Prince, and you've got quite a capable first gen satellite launcher.
True, trouble is it's a bit too early. An operational satellite launcher in 1965 merely allows the UK to spend even more money having to develop satellites to fly on it. By the early '70s, that would still be necessary, but they might also attract European partners and/or some overseas customers.
 
Joshuapooleanox wrote:
With a POD of 1945, have Britain and its Commonwealth be a key player in the Space Race with both the United States and the Soviet Union, possibly as a 3rd power.

Money and politics but ain't that always the case? :)

Riain wrote:
Blue Streak comes up a lot in British space/nuclear discussion and I think there is a lot of misconception surrounding it, someone (me?) really should gather some definitive stuff together and put it in my British cold war facts and figures thread.

While the Blue Streak itself was almost a 2//3 scale version of the Atlas its intended mode of operation and thus utility and longevity as a deterrent were vastly better. The Blue Streak was always fully fueled in its silo, but the LOX tank was filled with pressurised nitrogen to keep thin-wall the missile rigid, each silo had a LOX tank which re-liquefied LOX boil-off and the LOX was 'blasted' into the oxidiser tank by compressed gas in 3 1/2 minutes. The missile was then launched directly from the silo (not hoisted to the surface like Atlas and Titan I), the blast doors being equipped with high pressure water jets to clear away any debris that might block its opening operation, within 4 1/2 minutes.

Once the LOX was on board the missile could be kept fully fueled and ready for 30 second launch for 10 hours, before having to be drained of LOX and made ready to repeat the process, the turnaround time for this process also being 10 hours. Thus in theory 50% of the Blue Steak force could be kept at 30 seconds notice to fire, which in deterrent terms is more than suitable.

However what II suspect would happen in practice is the time on 30 second alert would creep up to maybe 12 hours, the time to turn around for the next 30 second alert would creep down to 8-9 hours and an intermediate stage of turnaround to 4 1/2 minutes to launch introduced, maybe 6 (?) hours. The result is a system that is considerably more flexible than Polaris and able to put up to 60% of its force on 30 seconds to launch or the whole force down to 4 1/2 minutes to launch and anything in between as the international diplomatic situation requires.

The upshot being that writing off a British space programme because Blue Streak is a piece of shit isn't really valid.
(Quoted for my records, thanks for the information!)

The problem wasn't the 'missile' it was the location. (See my first response to the OP :) ) As noted in/at "A Vertical Empire" the "best" place for the Blue Streak silo's was the one place they probably couldn't be located (http://www.spaceuk.org/bstreak/bs/k11.html) which drove the search for 'other' options which lead to Polaris and submarines. In essence the Brit's were ahead of the game technically in most areas, but they had a lot more going on a falling budget to contend with that stoppered many advanced plans.

As noted the key here is an actual 'need' which presupposes some changes in both decisions as well as financing. Blue Streak worked as a booster, (even as the booster for Europa, the BS worked) and it could be augmented as time went on.

Lots of interesting Blue Streak info here:
https://www.secretprojects.co.uk/forum/index.php/topic,9074.0/all.html
(But then again EVERYTHING there is "interesting" so be warned :) )

Stas-200 wrote:
There's nothing wrong with hypergols or solids on a launch vehicle (e.g. Ariane 1-4, Titan, Proton, Dnepr, Scout, all of Delta except the core), plus all of the early Indian and Chinese launchers.
From a modern perspective, most hypergols are fairly nasty and you wouldn't design a launcher today to use them, but anything that's good for an operational missile with a solid service history is a great basis for an early launcher.

That last part is the key here in that Blue Streak with a good upper stage was quite capable of competing with the likes of launchers like the Atlas-Agena. Constant upgrading could result in a pretty steady run as an LV.

If you want Blue Streak to stand a chance of entering service, you probably have to avoid Skybolt altogether - it was too cheap and credible an alternative (or so it seemed).

Blue Steel had already given a 'taste' of what was possible with an air-launched missile, that it wasn't all that GOOD of a "missile" was actually beside the point :) (Oddly enough I've seen some stuff on SPF that shows a "Blue Steel MKII" with ramjets right where I'd expect them) In essence both the RAF and USAF were 'interested' in ALBM but, (especially in the US) they didn't make as much sense as the bigger and more capable ICBMs. It actually DID make sense for Britain due to its circumstances, (as did Polaris) but having the US pay for the majority of development was icing on the cake. Having the US 'not interested' ups the needed commitment but doesn't address the basic issues.

Having to have the early Blue Steel "test" vehicle manned, (as the electronics and guidance aren't quite there yet) could add some 'low-hanging-fruit' first to keep the British sun from setting as quickly as OTL.

Putting Blue Streak into service and then phasing it out in the late '60s has possibilities though, as it might provide surplus missiles and infrastructure.

And that much more likely to "need" a way to transition the infrastructure and hardware into an operational LV. Still the main question is where do you put the things?

True, trouble is it's a bit too early. An operational satellite launcher in 1965 merely allows the UK to spend even more money having to develop satellites to fly on it. By the early '70s, that would still be necessary, but they might also attract European partners and/or some overseas customers.

THE problem with being 'first' is you have to pay a lot more than those who come later :) Specifically British electronics and other 'subsidiary' industries were having issues keeping up with what they actually NEEDED, (see Blue Steel above) rather than what they might want. And getting up to speed cost money and time they didn't really have.

Randy
 

Thomas1195

Banned
British electronics and other 'subsidiary' industries
Which were already crap as an industry as a whole (like most British high-tech industries) (although it managed to hold an artificial leadership in Europe for a while because Germany was ruined by ww2) and lagged behind America from the beginning.
 
Which were already crap as an industry as a whole (like most British high-tech industries) (although it managed to hold an artificial leadership in Europe for a while because Germany was ruined by ww2) and lagged behind America from the beginning.

I'll be first in line to crap over what Lucas did on the Consumer end, but Marconi and BAe mostly had their act together
 
H2O2/kerosine are quite storable propellants and they are much, much easier to handle (also they're cheaper)
Important if you're presuming a military spinoff as your basic lifter. Don't forget, tho, specific impulse is an issue for lifting commercial payloads, & AIUI, the solids aren't as good in that regard.
 
Important if you're presuming a military spinoff as your basic lifter. Don't forget, tho, specific impulse is an issue for lifting commercial payloads, & AIUI, the solids aren't as good in that regard.

For the upper stage, true. Though it is possible to just use a bigger keroxide upper stage. If high performance is needed really needed, they could do what the Americans did and use a different fuel and propellant on the final stage - like H2/O2, or go with UDMH/H2O2 (which has a higher specific impulse and is also hypergolic, simplifying the design of the upper stage and increasing reliability).

I wonder if the US would be willing to sell the UK Centaur upper stages?

fasquardon
 
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I wonder if the US would be willing to sell the UK Centaur upper stages?

fasquardon

Hawker-Siddeley briefly studied it late in the BSSLV saga, but by that stage the whole project was so far out of favour that it was never going to happen. I don't believe they ever got as far as taking to the Americans, although I suspect that reasons not to do it would have been found in the US. With a couple of strapon motors, Blue Streak-Centaur could have been an unwelcome competitor for both Delta and Atlas.
 
I don't claim expertise, but it's not clear to me why higher Isp isn't desirable from Stage 1: better Isp means lower fuel fraction means more payload.

Stage 1 needs to deal with more gravity drag, so denser fuels (which need less tankage) and higher thrust are more desirable than ISP - H2O2 is the densest oxidizer - at least, the densest one that is easy to handle.

The same is true of single stage to orbit vehicles, where H2 and LOX, with their excellent ISP, turn out to be a really poor choice of propellants because the huge hydrogen tanks push the dry mass through the roof.

Hawker-Siddeley briefly studied it late in the BSSLV saga, but by that stage the whole project was so far out of favour that it was never going to happen. I don't believe they ever got as far as taking to the Americans, although I suspect that reasons not to do it would have been found in the US. With a couple of strapon motors, Blue Streak-Centaur could have been an unwelcome competitor for both Delta and Atlas.

True.

fasquardon
 
That makes sense, except, I understood high thrust & high Isp were synonymous. Not so?
No, high ISp tends to mean lots of hydrogen in the fuel (LH2, methane is CH4, etc) which tend to mean lower densities, both in the tanks and in the engine itself. That meas larger engines physically for the same mass flow, and thus lower T/W engines and lower efficiency (prop kg/tank kg) tanks. It's a balancing act, and one reason methane/LOX has been seeing a lot of interest lately is being better than kerolox on delivered ISp while having a density more like it than hydrogen/LOX.
 
Warren Ellis' graphic novel Ministry of Space addresses this theme.. It's an interesting read, if more than a a bit improbable.

SPOILERS:

Britain reaches Peenemunde before the Americans and Soviets and gets all the scientists for themselves. Britain builds itself an Empire in space while keeping the Americans and Soviets Earth-bound. By 2001, the UK has the "Dan Dare" future, but is socially static, still racially segregated, even in space. The story ends with the UK's dark secret on the verge of exposure: The whole thing was funded with gold the Nazis looted from Holocaust victims, which the British confiscated and kept for themselves.
The fact the Soviets aren't a major player is a major flaw of the book. Not only did the Soviets largely depend on domestic talent for their rockets, but the fact the British just do the space program rather than are prompted to do so for prestige is suspicious.
 
No, high ISp tends to mean lots of hydrogen in the fuel (LH2, methane is CH4, etc) which tend to mean lower densities, both in the tanks and in the engine itself. That meas larger engines physically for the same mass flow, and thus lower T/W engines and lower efficiency (prop kg/tank kg) tanks. It's a balancing act, and one reason methane/LOX has been seeing a lot of interest lately is being better than kerolox on delivered ISp while having a density more like it than hydrogen/LOX.
Huh. So all this time, my focus on high Isp was (at least in part) in error.:frown: (I blame Jerry Pournelle.:openedeyewink:)

Thx for straightening me out.:)
 
Huh. So all this time, my focus on high Isp was (at least in part) in error.:frown: (I blame Jerry Pournelle.:openedeyewink:)

To be fair, it's been a common mistake to pursue ISP to the point of impracticality - it's why the Americans put most of their R&D into hydrogen fueled engines from 1970 on.

It's a balancing act, and one reason methane/LOX has been seeing a lot of interest lately is being better than kerolox on delivered ISp while having a density more like it than hydrogen/LOX.

I thought the principal reasons for the interest in methane is that the world is running out of oil that can be made into RP-1 and the interest by some in manufacturing methane on Mars.

fasquardon
 
Important if you're presuming a military spinoff as your basic lifter. Don't forget, tho, specific impulse is an issue for lifting commercial payloads, & AIUI, the solids aren't as good in that regard.
Why aren't they is good?
 
Why aren't they is good?
I would have given you an answer based on lower overall Isp against liquids, plus (perhaps) the inability to shut them off, but the first part is incorrect & I suspect the second is more/less moot...
 
Listening to the audiobook of "Cosmos" and he mentions us having launched a satellite and this made me sad
 
For the upper stage, true. Though it is possible to just use a bigger keroxide upper stage. If high performance is needed really needed, they could do what the Americans did and use a different fuel and propellant on the final stage - like H2/O2, or go with UDMH/H2O2 (which has a higher specific impulse and is also hypergolic, simplifying the design of the upper stage and increasing reliability). I wonder if the US would be willing to sell the UK Centaur upper stages?
Westcott developed the Delta which was a kerosene and liquid oxygen engine, it was rendered superfluous when North American Aviation's subsidiary Rocketdyne licensed their S-3 to Rolls-Royce as the RZ1. NAA and Rolls-Royce apparently had good relations from their previous dealings from the development of the Mustang, it's been suggested that they did the S-3/RZ1 deal mostly on a handshake, so it's certainly not outside the realm of possibility that they also license the RL10 engine provided that the US government didn't intervene.

I'd need to go back and check but IIRC the British also did a fair amount of their own research on liquid hydrogen and liquid oxygen engines, going so far as to test fire various chamber designs. They never built any full rocket stages for use though.
 
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