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
Co-axial turboramjet
Notional LH2-fuelled ramjet engine. Study 1985. Used on Sanger II launch vehicle.

Status: Study 1985. Thrust: 250.00 kN (56,200 lbf). Specific impulse: 1,200 s. Specific impulse sea level: 3,600 s. Burn time: 6,565 s.

Thrust (sl): 750.000 kN (168,600 lbf). Thrust (sl): 76,476 kgf.

Family: Ramjet. Country: Germany. Launch Vehicles: Saenger II. Propellants: Air/LH2. Stages: Sanger II-1.
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