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Dynasoar 4

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X-20 Dynasoar
X-20 Dynasoar at sunrise
Credit: © Mark Wade

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Launched: 1966 Late. Number crew: 1 .

Orbital attitude maneuvers would have been made to plus/minus 90 degrees in all axes, including visual reference checks. During re-entry control maneuvers would be made at pitch angles of from 10 to 50 degrees with a 3000 m altitude margin.

• Dynasoar 4 (cancelled) - . Nation: USA. Flight: Dynasoar 4. Spacecraft: Dynasoar. Planned date for second manned Dynasoar single-orbit flight..