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
Scramjet
Scram. Development ended 1992. Thrust is maximum sea level thrust; specific impulse is average during ascent. Propellant Slush LH2.

Status: Development ended 1992. Thrust: 1,372.90 kN (308,640 lbf). Specific impulse: 1,550 s. Burn time: 886 s. Diameter: 16.00 m (52.00 ft).

Thrust (sl): 1,372.900 kN (308,640 lbf). Thrust (sl): 140,000 kgf.



Country: USA. Engines: Scramjet. Launch Vehicles: Tu-2000, X-30. Propellants: Air/Slush LH2. Stages: Tu-2000 EAP.

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