Author Topic: ISRO Hybrid Rocket Engine Technology - General Discussion  (Read 21235 times)

Offline vyoma

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ISRO study on Hybrid Rocket Engine Technology:
1) Solid fuel (HTPB, Paraffin, PVC, PMMA, PU, PP).
2) Liquid oxidizer (LOX, GOX, H2O2, N2O, N2O4, Liquid Flourine).
3) Can throttle solid motor and control the thrust to achieve very precise missions.
4) Development program currently working only on sounding rockets.


Source:
« Last Edit: 07/31/2022 06:40 pm by vyoma »

Offline JayWee

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Re: Hybrid Rocket Engine Technology - General Discussion
« Reply #1 on: 07/23/2022 09:32 pm »
Hmm, judging by the troubles Virgin Galactic had with their engine - had to introduce methane+helium to make it stable, I'm not sure hybrid engines are the way to go.

Offline vyoma

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Re: Hybrid Rocket Engine Technology - General Discussion
« Reply #2 on: 07/23/2022 10:42 pm »
Hybrid engine (LOX/HTPB) demonstration in sounding rocket.

 

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