Dynasoar 10

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

Dynasoar 10

Part of Dynasoar

Dyna Soar
Credit: USAF

Planned eighth manned flight, second multi-orbit flight, and final flight of the Dynasoar program would have the objectives to demonstrate maneuver in orbit and during re-entry, and a precision recovery. Project cancelled in December 1963

Launched: 1968 Early. Number crew: 1 .

The inclination of the orbit would be adjusted three degrees using the transtage engine. During re-entry sustained flight would be made near the thermal limits of the spacecraft demonstrating an 1850 km cross-range capability.

Country: USA. Bibliography: 152, 583.

Dynasoar 10 (cancelled) - . Nation: USA. Flight: Dynasoar 10. Spacecraft: Dynasoar. Planned date for eighth manned flight, second multi-orbit flight, and final flight of the Dynasoar program..

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