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Three hours before dawn, Gene Kranz’ White Team took its place next to Windler’s Maroon Team controllers. The eighty hours of uncertainty were now past and mission control was down to Apollo 13’s final shift.
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Apollo Saturn 201 employed the Saturn IB launch vehicle, which was the up-rated version of the Saturn I rocket flown in ten earlier Saturn-Apollo missions. It featured an upgrade of the first stage engines to increase thrust from 1,500,000 lb-ft of thrust to 1,600,000 lb-ft. The second stage was the S-IVB. This stage used a new liquid hydrogen-burning J-2 engine which would also be used on the S-II second stage of the Saturn V lunar launch vehicle…
AS-201 Recovery
Apollo-Saturn 201 Launch
AS-202 Launch
AS-203 Launch
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The Pegasus satellite was named for the winged horse of Greek mythology. Like its namesake, the Pegasus was notable for its “wings”, a pair of 29 meter long, 4.3 meter wide arrays of 104 panels fitted with sensors to detect punctures by micrometeoroids at high altitudes. In its stored position with panels folded inside the Apollo service module, the Pegasus was 5.3-meters high, 2.1 meters wide, and 28-cm deep.
Pegasus Stowed Inside the Boilerplate Service Module
Pegasus Micrometeoroid Detection Satellite Deployed
Pegasus Deployment Sequence
SA-9 Launch
SA-8 Launch
SA-10 Launch
Interior of Command Module
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Since the lunar module would fly only in space (earth orbit and lunar vicinity), the designers could ignore the aerodynamic streamlining demanded by earth’s atmosphere and build the first true manned spacecraft, designed solely for operating in the spatial vacuum.
Lunar module generations from 1962 to 1969
James Webb examines models of the LEM and CM
Underside of LEM descent stage shows fuel tank installation
LEM Descent Stage
Mockup of LEM cabin with seats
1964 Version of LEM, No Seats and Triangular windows
LEM Sleep Stations
