Pegasus 1
American satellite
title: "Pegasus 1" type: doc version: 1 created: 2026-02-28 author: "Wikipedia contributors" status: active scope: public tags: ["spacecraft-launched-in-1965", "spacecraft-launched-by-saturn-rockets"] description: "American satellite" topic_path: "general/spacecraft-launched-in-1965" source: "https://en.wikipedia.org/wiki/Pegasus_1" license: "CC BY-SA 4.0" wikipedia_page_id: 0 wikipedia_revision_id: 0
::summary American satellite ::
::data[format=table title="Infobox spaceflight"]
| Field | Value |
|---|---|
| name | Pegasus 1 |
| image | Pegasus satellite.jpg |
| image_caption | A Pegasus satellite in orbit |
| mission_type | Micrometeoroid detection |
| operator | NASA |
| COSPAR_ID | 1965-009A |
| SATCAT | 001085 |
| mission_duration | 3 years 6 months 13 days |
| spacecraft_type | Pegasus |
| manufacturer | Fairchild Hiller |
| launch_mass | 10297 kg |
| payload_mass | 1450 kg |
| launch_date | |
| launch_rocket | Saturn I SA-9 |
| launch_site | Cape Canaveral LC-37B |
| disposal_type | Decommissioned |
| deactivated | |
| decay_date | 17 September 1978 |
| orbit_epoch | 18 March 1965 |
| orbit_reference | Geocentric |
| orbit_regime | Low Earth orbit |
| orbit_periapsis | 500 km |
| orbit_apoapsis | 731 km |
| orbit_inclination | 31.7 degrees |
| orbit_period | 97.00 minutes |
| apsis | gee |
| programme | Apollo micrometeoroid investigation |
| next_mission | Pegasus 2 |
| :: |
| name = Pegasus 1 | image = Pegasus satellite.jpg | image_caption = A Pegasus satellite in orbit
| mission_type = Micrometeoroid detection | operator = NASA | website = | COSPAR_ID = 1965-009A | SATCAT = 001085 | mission_duration = 3 years 6 months 13 days
| spacecraft_type = Pegasus | manufacturer = Fairchild Hiller | dry_mass = | launch_mass = 10297 kg | payload_mass = 1450 kg | power =
| launch_date = | launch_rocket = Saturn I SA-9 | launch_site = Cape Canaveral LC-37B | launch_contractor =
| disposal_type = Decommissioned | deactivated = | decay_date = 17 September 1978
| orbit_epoch = 18 March 1965 | orbit_reference = Geocentric | orbit_regime = Low Earth orbit | orbit_periapsis = 500 km | orbit_apoapsis = 731 km | orbit_inclination = 31.7 degrees | orbit_period = 97.00 minutes | apsis = gee
| programme = Apollo micrometeoroid investigation | previous_mission = | next_mission = Pegasus 2 Pegasus 1 or I, known before launch as Pegasus A, was an American satellite which was launched in 1965 to study micrometeoroid impacts in low Earth orbit. It was the first of three Pegasus satellites to be launched. The Pegasus spacecraft were manufactured by Fairchild Hiller, and operated by NASA.
Spacecraft
::figure[src="https://upload.wikimedia.org/wikipedia/commons/b/b8/Pegasus-1_satellite_is_installed_on_top_of_a_Saturn_I_rocket.jpg" caption="Pegasus-1, meteoroid detection satellite, installed on Saturn I (SA-9 mission) S-IV stage, January 13, 1965."] ::
Pegasus 1 was a Pegasus satellite, consisting of 1450 kg of instruments, attached to the S-IV upper stage of the carrier rocket which had placed it into orbit. It had a total mass of 10297 kg, and was equipped with two sets of micrometeoroid detection panels, and a radio for tracking and returning data. The panels were 29 m long, and equipped with 116 individual detectors.
Launch
::figure[src="https://upload.wikimedia.org/wikipedia/commons/8/8b/Saturn_SA9_launch.jpg" caption="The launch of Pegasus 1"] ::
Pegasus 1 was launched atop a Saturn I rocket, serial number SA-9, flying from Launch Complex 37B at the Cape Kennedy Air Force Station. The launch occurred at 14:37:03 UTC on 16 February 1965. Following launch, Pegasus 1 was given the COSPAR designation 1965-009A, while NORAD assigned it the Satellite Catalog Number 01085.
Pegasus 1 was a secondary payload of Apollo program mission AS-103, which also carried a boilerplate Apollo spacecraft BP-16. The Apollo boilerplate acted as a payload fairing for the Pegasus spacecraft, which was stored inside what would have been the Service Module of a functional spacecraft. Upon reaching orbit, the boilerplate Command and Service modules were jettisoned.
The trajectory and space-fixed velocity were very nearly as planned. The Apollo shroud separated from the Pegasus satellite about 804 seconds after lift-off and deployment of two meteoroid detection panel wings of the Pegasus satellite commenced about 1 minute later.
Operations
Pegasus 1 was operated in a low Earth orbit. On 18 March 1965 it was catalogued as being in an orbit with a perigee of 500 km and an apogee of 731 km, inclined at 31.7 degrees to the Equator and with a period of 97.00 minutes. Once in orbit, the panels were deployed to detect micrometeoroid impacts. Experiment results were returned to Earth by radio. The spacecraft operated until 29 August 1968, and subsequently remained in orbit until it decayed and reentered the atmosphere on 17 September 1978. Although minor malfunctions occurred in both the launch vehicle and the satellite, the mission was a success in that all objectives were met.
References
References
- Krebs, Gunter. "Pegasus 1, 2, 3". Gunter's Space Page.
- "World Civil Satellites 1957-2006". Space Security Index.
- Wade, Mark. "Pegasus".
- McDowell, Jonathan. "Launch List". Jonathan's Space Page.
- McDowell, Jonathan. "Launch Log". Jonathan's Space Page.
- "Pegasus 1". US National Space Science Data Center.
- McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page.
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