Bloodhound LSR Thread As Requested...
Discussion
CraigyMc said:
slartibartfast said:
he seemed to skip what they are going to use instead of the Jag V8 to pump rocket fuel.
£12m and it runs.
Fairly straightforward to do it with an electric motor.£12m and it runs.
Gareth79 said:
CraigyMc said:
slartibartfast said:
he seemed to skip what they are going to use instead of the Jag V8 to pump rocket fuel.
£12m and it runs.
Fairly straightforward to do it with an electric motor.£12m and it runs.
loudlashadjuster said:
I recall they’d already swapped the Jag V8 for another, more modest engine before the planned switch to electric?
Jaguar were an initial sponsor, but that didn’t last until the SA shakedown so I think it had been replaced by then.
Other way round IIRC. Jaguar were an initial sponsor, but that didn’t last until the SA shakedown so I think it had been replaced by then.
The Jag engine replaced something else, possibly a Cosworth F1 engine.
CraigyMc said:
slartibartfast said:
he seemed to skip what they are going to use instead of the Jag V8 to pump rocket fuel.
£12m and it runs.
Fairly straightforward to do it with an electric motor.£12m and it runs.
Edited by CallMeLegend on Monday 20th November 15:08
ChocolateFrog said:
loudlashadjuster said:
I recall they’d already swapped the Jag V8 for another, more modest engine before the planned switch to electric?
Jaguar were an initial sponsor, but that didn’t last until the SA shakedown so I think it had been replaced by then.
Other way round IIRC. Jaguar were an initial sponsor, but that didn’t last until the SA shakedown so I think it had been replaced by then.
The Jag engine replaced something else, possibly a Cosworth F1 engine.
Fundamentally any ICE unit is unsuitable, you have to get supersonic air in, slow it to manageable speeds, which heats it up, so you also have to cool it before the ICE gets to use it. Then you have the issues of dealing with exhaust gasses, so you are looking for the lowest pressure area in the under floor so perforate to have a suitable exhaust exit. Problem is these low pressure areas can move through the speed range.
Edited by CallMeLegend on Monday 20th November 15:27
CallMeLegend said:
CraigyMc said:
slartibartfast said:
he seemed to skip what they are going to use instead of the Jag V8 to pump rocket fuel.
£12m and it runs.
Fairly straightforward to do it with an electric motor.£12m and it runs.
Edited by CallMeLegend on Monday 20th November 15:08
Seems a transferrable skill
CraigyMc said:
CallMeLegend said:
CraigyMc said:
slartibartfast said:
he seemed to skip what they are going to use instead of the Jag V8 to pump rocket fuel.
£12m and it runs.
Fairly straightforward to do it with an electric motor.£12m and it runs.
Edited by CallMeLegend on Monday 20th November 15:08
Seems a transferrable skill
Olivergt said:
What does/did the jet use to supply fuel to the engine? Surely the requirements are the same, why not use the same?
Have just seen this post.The EJ200 has an AMAD (basically a jet-engine powered alternator) but it's sized for the fighter the engine came from; the rocket motor pump power requirement is quite a bit bigger; I recall this being discussed years ago; it's in the hundreds of kW (~400 to 500).
This is historical info but:
- The oxidiser pump needs to dump 800 litres of HTP into the rocket in a total of about 17s.
- HTP's a bit denser than water, that 800 litres equates to about 1000kg.
If you're looking to visualise the output of the pump, it's roughly equivalent to 15 UK-spec firefighting hoses running in parallel, in terms of flow rate.
If you were to dump the HTP out through a tube (unburnt) rather than as the oxidiser for a PBAN rocket, it'd still give you about 400lb of thrust. This is simply because of the reaction mass of the HTP going out the back of the car.
That's why the jet can't power the pump. Too squirty.
Edited by CraigyMc on Monday 20th November 20:14
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