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Pegasus 1

American satellite

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

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

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

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

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.

Info: Wikipedia Source

This article was imported from Wikipedia and is available under the Creative Commons Attribution-ShareAlike 4.0 License. Content has been adapted to SurfDoc format. Original contributors can be found on the article history page.

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