Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Lox/C3H8
Lox/C3H8 propellant. C3H8 liquid propane was proposed as a more 'environmentally friendly' rocket fuel in Russia in the 1990's, and was tested in place of kerosene in some test engines, but no such engine reached production.

Density: 0.493 g/cc. Boiling Point: -44 deg C.



Subtopics

AirLaunch Propane Engine Air Launch LOx/Propane rocket engine. Flow calibration, ignition and initial short duration tests completed in 2005 of this upper stage rocket engine with application to future small spacecraft launchers.

Engines: AirLaunch Propane Engine.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2017 Mark Wade - Contact
© / Conditions for Use