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Dynasoar 9
Part of Dynasoar
Dyna Soar
Dyna Soar
Credit: USAF
Planned first multi-orbit flight and seventh manned flight of Dynasoar would have the objectives to demonstrate maneuver in orbit and during re-entry, and a precision recovery. Project cancelled in December 1963

Launched: 1967 December. Number crew: 1 .

The apogee of the orbit would be adjusted using the transtage engine. During re-entry sustained flight would be made near the thermal limits of the spacecraft, at pitch angles of 40 degrees and roll angles of plus/minus 30 degrees.



Country: USA. Bibliography: 152, 583.

1967 December - .

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