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Pegasus 3 or III, also known as Pegasus C before launch, was an American satellite which was launched in 1965 to study micrometeoroid impacts in Low Earth orbit. It was the last of three Pegasus satellites to be launched, the previous two having been launched earlier the same year. It was manufactured by Fairchild Hiller, and operated by NASA.
Art, Launch & Operations
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pegasus orbit launch spacecraft micrometeoroid earth 1965 launched rocket satellite low nasa operated boilerplate apollo also kilograms lb payload 95
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Pegasus 3 | Apogee altitude | 536 kilometers (333 mi) | 1.00 | infobox |
| Pegasus 3 | COSPAR ID | 1965-060A | 1.00 | infobox |
| Pegasus 3 | Deactivated | 29 August 1968 (1968-08-30) | 1.00 | infobox |
| Pegasus 3 | Decay date | 4 August 1969 | 1.00 | infobox |
| Pegasus 3 | Disposal | Decommissioned | 1.00 | infobox |
| Pegasus 3 | Epoch | 3 September 1965 | 1.00 | infobox |
| Pegasus 3 | Inclination | 28.8 degrees | 1.00 | infobox |
| Pegasus 3 | Launch date | 30 July 1965, 13:00:00 (1965-07-30UTC13Z) UTC | 1.00 | infobox |
| Pegasus 3 | Launch mass | 10,323 kilograms (22,758 lb) | 1.00 | infobox |
| Pegasus 3 | Launch site | Cape Canaveral LC-37B | 1.00 | infobox |
| Pegasus 3 | Manufacturer | Fairchild Hiller | 1.00 | infobox |
| Pegasus 3 | Mission duration | 1 year (design) 3 years (achieved) | 1.00 | infobox |
| Pegasus 3 | Operator | NASA | 1.00 | infobox |
| Pegasus 3 | Payload mass | 1,450 kilograms (3,200 lb) | 1.00 | infobox |
| Pegasus 3 | Perigee altitude | 516 kilometers (321 mi) | 1.00 | infobox |
| Pegasus 3 | Period | 95.15 minutes | 1.00 | infobox |
| Pegasus 3 | Reference system | Geocentric | 1.00 | infobox |
| Pegasus 3 | Regime | Low Earth | 1.00 | infobox |
| Pegasus 3 | Rocket | Saturn I SA-10 | 1.00 | infobox |
| Pegasus 3 | SATCAT no. | 01467 | 1.00 | infobox |
| Pegasus 3 | Spacecraft type | Pegasus | 1.00 | infobox |
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