Saturn V SA-513 (Skylab-1) was launched at 13:30:00 Eastern Daylight Time (EDT) on May 14, 1973, from Kennedy Space Center, Complex 39, Pad A. The vehicle lifted off on a launch azimuth of 90 degrees east of north and rolled to a flight azimuth of 40.88 degrees east of north. The launch vehicle successfully placed the Saturn Work Shop in the planned earth orbit. All launch vehicle objectives were accomplished. No launch vehicle failures or anomalies occurred that seriously affected the mission
The launch vehicle stages for SL-2, the CSM experiments, and their associated support equipment are ...
Saturn/Apollo Uprated Saturn I launch development mission to test behavior of liquid hydrogen fuel d...
A Saturn 1B Flight Manual provides launch vehicle systems descriptions and predicted performance dat...
The performance evaluation of the SA-206 launch vehicle for the Skylab 2 launch is presented. Flight...
The results of the Saturn 1B, SA-208 launch vehicle flight evaluation are presented. The performance...
A postflight analysis of the Apollo 14 flight is presented. The basic objective of the flight evalua...
Evaluation results of prelaunch countdown, powered flight, and orbital phase of Saturn S-4B-501 laun...
The Skylab's Saturn Workshop mission performance is presented. Experiments were conducted to determi...
Advanced post-Saturn earth launch vehicle design and chemonuclear propulsion system performanc
Saturn I launch vehicle, Saturn IB launch vehicle, and Saturn V launch vehicle components and con...
Systems analyses, prelaunch countdown, powered flight, and orbital phases of Saturn-4B-504
The postflight trajectory for the Apollo/Saturn V SA-513 Skylab I flight is presented. An analysis i...
Revisions to the Apollo/Saturn 5 Launch Vehicle test and operations catalog sheets are presented. Th...
Trajectory and dynamics analyses of Saturn 1B launch vehicle for Apollo-Saturn 205/CSM-101 missio
Six degree of freedom trajectory analysis of Saturn 1B for Apollo-Saturn 204/LM-1 missio
The launch vehicle stages for SL-2, the CSM experiments, and their associated support equipment are ...
Saturn/Apollo Uprated Saturn I launch development mission to test behavior of liquid hydrogen fuel d...
A Saturn 1B Flight Manual provides launch vehicle systems descriptions and predicted performance dat...
The performance evaluation of the SA-206 launch vehicle for the Skylab 2 launch is presented. Flight...
The results of the Saturn 1B, SA-208 launch vehicle flight evaluation are presented. The performance...
A postflight analysis of the Apollo 14 flight is presented. The basic objective of the flight evalua...
Evaluation results of prelaunch countdown, powered flight, and orbital phase of Saturn S-4B-501 laun...
The Skylab's Saturn Workshop mission performance is presented. Experiments were conducted to determi...
Advanced post-Saturn earth launch vehicle design and chemonuclear propulsion system performanc
Saturn I launch vehicle, Saturn IB launch vehicle, and Saturn V launch vehicle components and con...
Systems analyses, prelaunch countdown, powered flight, and orbital phases of Saturn-4B-504
The postflight trajectory for the Apollo/Saturn V SA-513 Skylab I flight is presented. An analysis i...
Revisions to the Apollo/Saturn 5 Launch Vehicle test and operations catalog sheets are presented. Th...
Trajectory and dynamics analyses of Saturn 1B launch vehicle for Apollo-Saturn 205/CSM-101 missio
Six degree of freedom trajectory analysis of Saturn 1B for Apollo-Saturn 204/LM-1 missio
The launch vehicle stages for SL-2, the CSM experiments, and their associated support equipment are ...
Saturn/Apollo Uprated Saturn I launch development mission to test behavior of liquid hydrogen fuel d...
A Saturn 1B Flight Manual provides launch vehicle systems descriptions and predicted performance dat...