The Wayback Machine - https://web.archive.org/web/20161228060118/http://astronautix.com/r/rbss.html
RBSS

Encyclopedia Astronautica
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
RBSS
American winged orbital launch vehicle. The Recoverable Booster Space System was a plan circulated in the early 1960's to use the XB-70 as a recoverable supersonic first stage for a range of systems. The XB-70 would be capable of orbiting a 6800 kg payload, or an X-20 manned space glider.
See More

AKA: Recoverable Booster Space System. Status: Study 1962. Payload: 6,800 kg (14,900 lb). Thrust: 519.00 kN (116,675 lbf). Gross mass: 230,000 kg (500,000 lb). Height: 56.40 m (185.00 ft). Diameter: 9.14 m (29.98 ft). Span: 32.01 m (105.01 ft). Apogee: 160 km (90 mi).

LEO Payload: 6,800 kg (14,900 lb) to a 160 km orbit at 90.00 degrees.

Family: aircraft-launched, orbital launch vehicle, Winged. Country: USA. Spacecraft: Dynasoar. Agency: North American. More at: 8534. Bibliography: 44.

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
� 1997-2016 Mark Wade - Contact
� / Conditions for Use