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
Sanger II-1
Mach 6.6 rocket launch aircraft. Winged scramjet using LH2 propellant. Releases Horus @M 6.6 @ 37 km altitude @ 3100 km range

AKA: EHTV;Sanger II. Status: Study 1985. Thrust: 1,500.00 kN (337,212 lbf). Gross mass: 254,000 kg (559,000 lb). Unfuelled mass: 156,000 kg (343,000 lb). Specific impulse: 1,200 s. Specific impulse sea level: 3,600 s. Burn time: 6,565 s. Height: 84.50 m (277.20 ft). Diameter: 14.00 m (45.00 ft). Span: 41.40 m (135.80 ft).

Cost $ : 10.000 million. No Engines: 6.



Country: Germany. Engines: Co-axial turboramjet. Launch Vehicles: Saenger II. Propellants: Air/LH2.

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