Pegasus satellite program

Pegasus satellite, attached to the S-IV upper stage
Manufacturer	Fairchild Hiller
Country of origin	United States
Operator	NASA
Applications	Micrometeoroid detection
Specifications
Launch mass	1,450 kilograms (3,200 lb)
Dimensions	29 meters (96 ft) wide by 4.1 meters (13.6 ft) long
Power	Solar cells
Regime	Low Earth orbit
Production
Status	retired
Built	3
Launched	3
Operational	16 February 1965
Retired	29 August 1968
Failed	0
First launch	16 February 1965
Last launch	30 July 1965
Deployment of a Pegasus Satellite

The Pegasus satellite program was a series of three American satellites launched in 1965 to study the frequency of micrometeorite impacts on spacecraft. All three Pegasus satellites were launched by Saturn I rockets, and remained connected with their upper stages.

The Pegasus satellite was named for the winged horse of Greek mythology and was first lofted into space by a NASA Saturn I rocket on February 16, 1965. Like its namesake, the Pegasus satellite was notable for its "wings", a pair of 96-foot (29 m)-long, 14-foot (4.3 m)-wide arrays of 104 panels fitted with sensors to detect punctures by micrometeoroids at high altitudes, in support of the Apollo Program to send manned lunar landing missions starting by 1970. Micrometeoroids were believed to be potentially hazardous to the Apollo crew if they could puncture the spacecraft skin. The sensors successfully measured the frequency, size, direction and penetration of scores of micrometeoroid impacts. The satellite also carried sample protective shields mounted on the arrays.

The NASA Marshall Space Flight Center was responsible for the design, production and operation of the three Pegasus satellites which were launched by Saturn I rocket test flights in 1965. At launch, a boilerplate Apollo Command/Service Module and launch escape system tower were atop the Saturn I, with the Pegasus experiment folded inside the Service Module. After first stage separation and second-stage ignition, the launch escape system was jettisoned. When the second stage attained orbit, the 10,000-pound Apollo boilerplate Command and Service modules were jettisoned into a separate orbit. Then a motor driven device extended the winglike panels on the Pegasus to a span of 96 feet (29 m). The Pegasus wings remained attached to the Saturn I's second stage as planned.

A television camera, mounted on the interior of the Service Module adapter, provided pictures of the satellite deploying in space and as one historian has written, "captured a vision of the eerie silent wings of Pegasus I as they haltingly deployed." The satellite exposed more than 2,300 square feet (210 m²) of instrumented surface, with thickness varying up to 0.016-inch (0.41 mm).