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
Albatros Carrier Aircraft
LOx/LH2 propellant rocket stage. Configuration: delta wing with wingtip vertical stabilizers and canards. Engine type and performance, empty weight estimated.

Status: Study 1974. Thrust: 7,840.00 kN (1,762,500 lbf). Gross mass: 1,250,000 kg (2,750,000 lb). Unfuelled mass: 210,000 kg (460,000 lb). Specific impulse: 455 s. Specific impulse sea level: 337 s. Burn time: 580 s. Height: 91.00 m (298.00 ft). Diameter: 7.00 m (22.90 ft). Span: 40.00 m (131.00 ft).

No Engines: 4.



Country: Russia. Engines: RD-0120. Spacecraft: Albatros. Propellants: Lox/LH2.

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