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
Truax LH2
Aerojet LOx/LH2 rocket engine. Test 1962. Used in Sea Horse-2.

Status: Test 1962. Thrust: 147.10 kN (33,069 lbf). Specific impulse: 425 s. Specific impulse sea level: 306 s. Burn time: 363 s. Diameter: 3.00 m (9.80 ft).

Thrust (sl): 105.900 kN (23,807 lbf). Thrust (sl): 10,800 kgf.



Country: USA. Launch Vehicles: Sea Horse. Propellants: Lox/LH2. Stages: Sea Horse-2. Agency: Aerojet.

Back to top of page
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
© 1997-2019 Mark Wade - Contact
© / Conditions for Use