Pioneer Venus Orbiter

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Pioneer Venus Orbiter
Pioneer Venus orbiter.jpg
Pioneer Venus Orbiter
Mission type Venus orbiter
Operator NASA  / ARC
COSPAR ID 1978-051A OOjs UI icon edit-ltr-progressive.svg
SATCAT no. 10911
Website Pioneer Venus at NASA
Mission duration14 years, 4 months, 18 days (from launch)
13 years, 10 months, 4 days (at Venus)
Spacecraft properties
Bus HS-507
Manufacturer Hughes
Launch mass582 kg (1,283 lb) [1]
Dry mass517 kg (1,140 lb)
Dimensions2.5 × 1.2 m (8.2 × 3.9 ft)
Power312 watts
Start of mission
Launch dateMay 20, 1978, 13:13:00 (1978-05-20UTC13:13Z) UTC [1]
Rocket Atlas SLV-3D Centaur-D1AR
Launch site Cape Canaveral LC-36A
End of mission
Last contactOctober 8, 1992, 19:22 (1992-10-08UTC19:23Z) UTC
Decay dateOctober 22, 1992 [2]
Orbital parameters
Reference system Cytherocentric
Semi-major axis 33,405.8 kilometres (20,757.4 mi)
Eccentricity 0.842
Pericytherion altitude 181.6 kilometers (112.8 mi)
Apocytherion altitude 66,630 kilometers (41,400 mi)
Inclination 105 degrees
Period 24 hours
Epoch 22 November 1979, 11:53:20 UTC [3]
Venus orbiter
Orbital insertionDecember 4, 1978
 

The Pioneer Venus Orbiter, also known as Pioneer Venus 1 or Pioneer 12, was a mission to Venus conducted by NASA as part of the Pioneer Venus project. Launched in May 1978 atop an Atlas-Centaur rocket, the spacecraft was inserted into an elliptical orbit around Venus on December 4, 1978. It returned data from Venus until October 1992. [2] [4]

Contents

Launch and arrival at Venus

Orbit attitude of Pioneer Venus 1 between 1978-1980 and 1992 Pioneer Venus 1 orbit attitude.gif
Orbit attitude of Pioneer Venus 1 between 1978–1980 and 1992

The Pioneer Venus Orbiter was launched by an Atlas SLV-3D Centaur-D1AR rocket, which flew from Launch Complex 36A at the Cape Canaveral Air Force Station. The launch occurred at 13:13:00 on May 20, 1978, and deployed the Orbiter into heliocentric orbit for its coast to Venus. Venus orbit insertion occurred on December 4, 1978.

Spacecraft

Pioneer Venus 1 at KSC. Pioneer Venus 1 at KSC.jpg
Pioneer Venus 1 at KSC.

Manufactured by Hughes Aircraft Company, the Pioneer Venus Orbiter was based on the HS-507 bus. [5] The spacecraft was a flat cylinder, 2.5 meters (8.2 ft) in diameter and 1.2 meters (3.9 ft) long. All instruments and spacecraft subsystems were mounted on the forward end of the cylinder, except the magnetometer, which was at the end of a 4.7 meters (15 ft) boom. A solar array extended around the circumference of the cylinder. A 1.09 metres (3 ft 7 in) despun dish antenna provided S and X band communication with Earth. A Star-24 solid rocket motor was integrated into the spacecraft to provide the thrust to enter orbit around Venus. [5]

From Venus orbit insertion to July 1980, periapsis was held between 142 and 253 kilometres (88 and 157 mi) (at 17 degrees north latitude) to facilitate radar and ionospheric measurements. The spacecraft was in a 24-hour orbit with an apoapsis of 66,900 kilometers (41,600 mi). Thereafter, the periapsis was allowed to rise to a maximum of 2,290 kilometres (1,420 mi) and then fall, to conserve fuel.

In 1991, the Radar Mapper was reactivated to investigate previously inaccessible southern portions of the planet, in conjunction with the recently arrived Magellan spacecraft. In May 1992, Pioneer Venus began the final phase of its mission, in which the periapsis was held between 150 and 250 kilometres (93 and 155 mi), until the spacecraft's propellant was exhausted, after which the orbit decayed naturally. The spacecraft continued to return data until 8 October 1992, with the last signals being received at 19:22 UTC. [4] The Pioneer Venus Orbiter disintegrated upon entering the atmosphere of Venus on October 22, 1992. [2]

Instruments

A map of Venus produced from Pioneer data Venus map with labels.jpg
A map of Venus produced from Pioneer data

The Pioneer Venus Orbiter carried 17 experiments with a total mass of 45 kilograms (99 lb): [6]

An image of Venus in ultraviolet light by the Pioneer Venus Orbiter Venus clouds seen by Pioneer Venus Orbiter.jpg
An image of Venus in ultraviolet light by the Pioneer Venus Orbiter
Orbit of the spacecraft Pioneer Venus Orbiter. Pioneer-Venus-Orbiter-orbit.png
Orbit of the spacecraft Pioneer Venus Orbiter.
Launch of Pioneer Venus Orbiter with Atlas-Centaur rocket. Atlas Centaur with Pioneer Venus Orbiter.jpg
Launch of Pioneer Venus Orbiter with Atlas-Centaur rocket.
Trajectory of Pioneer Venus Orbiter. Pioneer-Venus-Trajectories.png
Trajectory of Pioneer Venus Orbiter.
Instrument details
NameComplete designationTypeManufacturerResponsible scientistMassElectrical consumption
OCPPOrbiter Cloud PhotopolarimeterPhoto polarimeterGISSJ. Hansen (later L. Travis)5 kg (11 lb)5.4 W
ORADOrbiter Radar Mapper InstrumentRadarMITG. Pettengill9 kg (20 lb)18 W
OIROrbiter Infrared RadiometerInfrared radiometerJPLF. Taylor5.9 kg (13 lb)5.2 W
OUVSOrbiter Ultraviolet SpectrometerUltraviolet spectrometerLASPA.I.F. Stewart3.1 kg (6.8 lb)1.7 W
ONMSOrbiter Neutral Mass SpectrometerNeutral mass spectrometerGSFCH. Neimann3.8 kg (8.4 lb)12 W
OPAOrbiter Plasma AnalyzerAnalzer plasmaARCJ. Wolfe (later A. Barnes)3.9 kg (8.6 lb)5 W
OMAGOrbiter MagnetometerMagnetometerUCLAC. Russell2 kg (4.4 lb)2.2 W
OEFDOrbiter Electric Field DetectorMeasure the electric fields of VenusTRWF. Scarf0.8 kg (1.8 lb)0.7 W
OETPOrbiter Electron Temperature ProbeElectron temperature gaugeGSFCL. Brace2.2 kg (4.9 lb)4.8 W
OIMSOrbiter Ion Mass SpectrometerIon mass spectrometerGSFCH. Taylor3 kg (6.6 lb)1.5 W
ORPAOrbiter Retarding Potential AnalyzerIon charge meterLPARLW. Knudsen2.8 kg (6.2 lb)2.4 W
OGBDOrbiter Gamma-Ray Burst DetectorGamma-ray burst detectorLASLW. Evans2.8 kg (6.2 lb)1.3 W
-Venus (ORO)Radio science-A. Kliore (JPL)-
Orbiter Dual-Frequency Experiments (OGPE)-T. Croft (SRI)
Atmospheric and Solar Wind Turbulence Experiment (OTUR)-T. Croft (JPL)
Orbiter Atmospheric Drag Experiment (OAD)-G. Keating (LRC)
Orbiter Internal Density Distribution Experiment (OIDD)-R. Phillips (JPL)
Orbiter Celestial Mechanics Experiment (OCM)-I. Shapiro (MIT)
LASP: Laboratory for Atmospheric and Space Physics (University of Boulder, Colorado); UCLA: University of California in Los Angeles; JPL: Jet Propulsion Laboratory; MIT: Massachusetts Institute of Technology; GSFC: Goddard Space Flight Center GISS: Goddard Institute for Space Studies; LRC: Langley Research Center; ARC: Ames Research Center; LASL: Los Alamos National Laboratory; SRI: Stanford Research Institute

The spacecraft conducted radar altimetry observations allowing the first global topographic map of the Venusian surface to be constructed.

The instruments can also be classified by what they are meant to measure or analyze: [7]

Observations of Comets

From its orbit of Venus, the Pioneer Venus Orbiter was able to observe Halley's Comet when it was unobservable from Earth due to its proximity to the sun during February 1986. UV spectrometer observations monitored the loss of water from the comet's nucleus at perihelion on February 9. [8]

The extended mission allowed the spacecraft controllers to make several comet observations that were never part of the original mission objectives. The tilt of the spacecraft was altered during these comet observations so that the Ultraviolet Spectrometer (OUVS) could view the comets rather than Venus. Comets Encke (April 13-16, 1984), Giacobini-Zinner (September 8-15, 1985), Halley (December 27, 1985 - March 9, 1986), Wilson (March 13 - May 2, 1987), NTT (April 8, 1987), and McNaught (November 19-24, 1987) were all observed in this way. [7]

See also

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References

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Science Magazine in year 1979 issue 4401