Small update on the new plan of attack. We are now pursuing the development of a gas generator cycle 5000 pound-force ablative keralox rocket engine. We are currently attempting to calculate all the parameters for such an engine. With one ablative chamber on hand for testing, a hydrostatic test to simulate run pressures is expected very soon. Tests of scaled-down turbine, pump and gas generator components will follow. Stay tuned.
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For the first turbopump we are building, one of the major items we wanted to develop was a common, reusable pump core that contains all of t... -
Small update on the new plan of attack. We are now pursuing the development of a gas generator cycle 5000 pound-force ablative keralox rocke...
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Designing a turbine for a turbopump is critical considering the work the pump will do is ultimately derived from the gas turbine ...
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