Pressure-fed engine
The pressure-fed engine is a class of rocket engine designs. A separate gas supply, usually helium, pressurizes the propellant tanks to force fuel and oxidizer to the combustion chamber. To maintain adequate flow, the tank pressures must exceed the combustion chamber pressure.
Pressure fed engines have simple plumbing and have no need for complex and occasionally unreliable
Care must be taken, especially during long burns, to avoid excessive cooling of the pressurizing gas due to
Spacecraft attitude control and orbital maneuvering thrusters are almost universally pressure-fed designs.[2] Examples include the Reaction Control (RCS) and the
Some launcher
The 1960s Sea Dragon concept by Robert Truax for a big dumb booster would have used pressure-fed engines.
Pressure-fed engines have practical limits on propellant pressure, which in turn limits combustion chamber pressure. High pressure propellant tanks require thicker walls and stronger materials which make the vehicle tanks heavier, thereby reducing performance and payload capacity. The lower stages of
Other vehicles or companies using pressure-fed engine:
- OTRAG (rocket)
- Quad (rocket) of Armadillo Aerospace
- XCOR EZ-Rocket of XCOR Aerospace
- Masten Space Systems
- Aquarius Launch Vehicle
- NASA's Project Morpheus prototype lander
- NASA Mighty Eaglemini lunar lander
- CONAE's Tronador II upper stage[citation needed]
- Copenhagen Suborbitals' Spica
See also
- Gas-generator cycle
- Combustion tap-off cycle
- Expander cycle
- Staged combustion cycle
References
- ^ a b "LM Descent Propulsion Development Diary". Encyclopedia Astronautica. Archived from the original on 6 June 2012. Retrieved 5 June 2012.
- ^ ISBN 0-89499-134-5.
- ^ "Falcon 1 Users Guide" (PDF). SpaceX. 2008-09-28. Archived from the original (PDF) on 2 October 2012. Retrieved 5 June 2012.