Verify operation of Lunar Module ascent and descent propulsion
systems. Evaluate Lunar Module staging. Evaluate S-IVB instrument
unit performance. All mission objects achieved.
Launch:
January 22, 1968, 05:48:08 pm EST. Launch Complex 37B, Eastern
Test Range, Cape Canaveral FL. Hold for 228 minutes when spacecraft
water boiler temperature rose higher than planned, caused by problem
in GSE freon supply, and a power supply in an output register in the
digital data-acquisition system failed.
Launch Weight: xxx,xxx lbs.
Orbit:
Altitude: 961km
Inclination: xxx degrees
Orbits: 4
Duration: Days, hours, min, seconds
Distance: miles
Landing:
No recovery.
Mission Highlights:
Apogee was 222 km at insertion, LM/S-IVB seperation, and after
first descent engine firing. Apogee was raised to 961 km after first
ascent engine firing. Perigee was 163 km at insertion, 167km at
separation, 171 after descent engine firing, and 172 km after ascent
engine firing.
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