...verify subsystem operation; to evaluate performance of the space vehicle Emergency Detection System ; to demonstrate mission support facilities and operations required for launch, mission conduct, and Command Module recovery. The schedule provides for a third unmanned flight using AS-503. (e) Command...

...verify subsystem operation ; to evaluate performance of the space vehicle Emergency Detection System ; to demonstrate mission support facilities and operations required for launch, mission conduct and Command Module recovery. The schedule provides for a third unmanned flight using AS-503. e. Command...

...verify subsystem operation; to evaluate performance of the space vehicle Emergency Detection System ; to demonstrate mission support facilities and operations required for launch, mission conduct and Command Module recovery. The schedule provides for a third unmanned flight using AS-503. e. Command...

...verify subsystem operation ; to evaluate performance of the space vehicle Emergency Detection System ; to demonstrate mission support facilities and operations required for launch, mission conduct and Command Module recovery. The schedule provides for a third unmanned flight using AS-503. e. Command...

...systems; evaluate performance of emergency detection system (EDS) in closed-loop configuration; and demonstrate mission support facilities and operations required for launch, mission conduct, and command module (CM) recovery. Launch vehicle Ist-stage performance was near nominal, but two of five...

...the sixth orbit. The descent stage re-entered the atmosphere over the Pacific Ocean on February 12. Spacecraft ground support equipment (GSE) systems...flight duration of 9 hours and 49.75 minutes. Apollo 6 attained all but one of its primary objectives. Restart of the S-IVB stage in orbit did not occur....

...4. Evaluate performance of the space vehicle EDS in a closed-loop configuration (accomplished). 5. Demonstrate mission support facilities and operations...required for launch, mission conduct, and CM recovery (accomplished). Apollo 7 (AS-205) (October 11, 1968) Primary Objectives (all achieved) 1. Demonstrate...

...4. Evaluate performance of the space vehicle EDS in a closed-loop configuration (accomplished). 5. Demonstrate mission support facilities and operations...required for launch, mission conduct, and CM recovery (accomplished). Apollo 7 (AS-205) (October 11, 1968) Primary Objectives (all achieved) 1. Demonstrate...

...substitution of program reader assembly (PRA) control for primary guidance during the propulsion burns. The second DPS burn was then commanded. The duration...flight duration of 9 hours and 49.75 minutes. Apollo 6 attained all but one of its primary objectives. Restart of the S-FVB stage in orbit did not occur....

...performance of the space vehicle emergency detection subsystem in open-loop configuration. Achieved. 4. Demonstrate mission support facilities and operations required for launch, mission conduct and command module recovery. Achieved. Spacecraft Mandatory Detailed Test Objectives 1 . M 1 . 1 : Demonstrate...