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FASA Gemini Titan 2 engine cuts off too early


dennislee

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I'm not sure about RSS/RO engines in general, but I do know that fuel pumps are not able to remove 100% of the propellant from a tank. I believe LEM's unusable propellant was around 250lbs - granted the tank had a capacity of 18,000lbs so that is a pretty small fraction.  It looks like the Titan II used the same fuel blend (hydrazine and nitrogen tetroxide) so I would expect a similar (or at least nonzero) waste proportion.  It's interesting that it tells you that you don't have ignitions, because hypergolic fuels like that don't require a designated igniter.  But I'm not a propulsion scientist, what do I know?

Again, not sure if this (tank waste) is modeled but from what I've read about RO I wouldn't be surprised if it were.

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