Pioneer Venus Orbiter Explained

Pioneer Venus Orbiter
Names List:Pioneer Venus 1
Pioneer 12
Mission Type:Venus orbiter
Operator:NASAAmes
Website:science.nasa.gov
Cospar Id:1978-051A
Satcat:10911
Mission Duration:14 years, 4 months, 18 days (from launch)
13 years, 10 months, 4 days (at Venus)
Spacecraft Bus:HS-507
Manufacturer:Hughes
Dimensions:2.5xx
Dry Mass:517kg (1,140lb)
Launch Mass:582kg (1,283lb) [1]
Power:312 watts
Launch Date: UTC
Launch Rocket:Atlas SLV-3D Centaur-D1AR
Launch Site:Cape Canaveral LC-36A
Disposal Type:Decommissioned
Last Contact: UTC
Decay Date:October 22, 1992[2]
Orbit Epoch:22 November 1979, 11:53:20 UTC[3]
Orbit Reference:Cytherocentric
Orbit Semimajor:33405.8km (20,757.4miles)
Orbit Periapsis:181.6km (112.8miles)
Orbit Apoapsis:66630km (41,400miles)
Orbit Inclination:105 degrees
Orbit Period:24 hours
Orbit Eccentricity:0.842
Apsis:cytherion
Interplanetary:
Type:orbiter
Arrival Date:December 4, 1978
Programme:Pioneer program
Previous Mission:Pioneer 11
Next Mission:Pioneer 13
Programme2:Pioneer Venus

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.

Launch and arrival at Venus

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 (8:13 a.m. local time) 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

Manufactured by Hughes Aircraft Company, the Pioneer Venus Orbiter was based on the HS-507 bus.[4] The spacecraft was a flat cylinder, 2.5m (08.2feet) in diameter and 1.2m (03.9feet) 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 4.7m (15.4feet) boom. A solar array extended around the circumference of the cylinder. A 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.

From Venus orbit insertion to July 1980, periapsis was held between 142kmand253kmkm (88milesand157mileskm) (at 17 degrees north latitude) to facilitate radar and ionospheric measurements. The spacecraft was in a 24-hour orbit with an apoapsis of 66900km (41,600miles). Thereafter, the periapsis was allowed to rise to a maximum of 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 150kmand250kmkm (90milesand160mileskm), 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.[5] The Pioneer Venus Orbiter disintegrated upon entering the atmosphere of Venus on October 22, 1992.

Instruments

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

Instrument details
scope=col Namescope=col Complete designationscope=col Typescope=col Manufacturerscope=col Responsible scientistscope=col Massscope=col Electrical consumption
OCPPOrbiter Cloud Photopolarimeter Photo polarimeter GISS J. Hansen (later L. Travis) 5kg (11lb) 5.4 W
ORADOrbiter Radar Mapper Instrument Radar MIT G. Pettengill 9kg (20lb) 18 W
OIROrbiter Infrared Radiometer Infrared radiometer JPL F. Taylor 5.9kg (13lb) 5.2 W
OUVSOrbiter Ultraviolet Spectrometer Ultraviolet spectrometer LASP A.I.F. Stewart3.1kg (06.8lb) 1.7 W
ONMSOrbiter Neutral Mass Spectrometer Neutral mass spectrometer GSFC H. Neimann 3.8kg (08.4lb) 12 W
OPAOrbiter Plasma Analyzer Analzer plasma ARC J. Wolfe (later A. Barnes) 3.9kg (08.6lb) 5 W
OMAG Orbiter Magnetometer Magnetometer UCLA C. Russell 2kg (04lb) 2.2 W
OEFDOrbiter Electric Field Detector Measure the electric fields of Venus TRW F. Scarf 0.8kg (01.8lb) 0.7 W
OETPOrbiter Electron Temperature Probe Electron temperature gauge GSFC L. Brace 2.2kg (04.9lb) 4.8 W
OIMSOrbiter Ion Mass Spectrometer Ion mass spectrometer GSFC H. Taylor 3kg (07lb) 1.5 W
ORPAOrbiter Retarding Potential Analyzer Ion charge meter LPARL W. Knudsen 2.8kg (06.2lb) 2.4 W
OGBDOrbiter Gamma-Ray Burst Detector Gamma-ray burst detector LASL W. Evans 2.8kg (06.2lb) 1.3 W
align="center" rowspan="6"-S and X-Band Radio Occultation Studies of the Atmosphere and Ionosphere oVenus (ORO) Radio science align="center"- A. Kliore (JPL) align="center" rowspan="6"-
Orbiter Dual-Frequency Experiments (OGPE) align="center"- T. Croft (SRI)
Atmospheric and Solar Wind Turbulence Experiment (OTUR) align="center"- T. Croft (JPL)
Orbiter Atmospheric Drag Experiment (OAD) align="center"- G. Keating (LRC)
Orbiter Internal Density Distribution Experiment (OIDD) align="center"- R. Phillips (JPL)
Orbiter Celestial Mechanics Experiment (OCM) align="center"- 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

References

Bibliography

External links

Notes and References

  1. Web site: Pioneer Venus Orbiter/Pioneer Venus 1/Pioneer 12 . NASA's Solar System Exploration website . December 1, 2022.
  2. Web site: Satellite Catalog . Jonathan. McDowell . Jonathan's Space Page . live . 2003-10-11 . https://web.archive.org/web/20031011062901/http://planet4589.org/space/log/satcat.txt .
  3. Web site: NASA - NSSDCA - Spacecraft - Trajectory Details. nssdc.gsfc.nasa.gov. 2018-05-02.
  4. Web site: Pioneer 12 (Pioneer Venus Orbiter, PVO) . Gunter . Krebs . Gunter's Space Page . live . 2005-01-12 . https://web.archive.org/web/20050112064044/http://space.skyrocket.de/doc_sdat/pioneer-12.htm .
  5. Web site: Pioneer Venus 1 . NASA . Solar System Exploration . dead . 2006-10-04 . https://web.archive.org/web/20061004114707/http://solarsystem.nasa.gov/missions/profile.cfm?Sort=Target&Target=Venus&MCode=Pioneer_Venus_01&Display=ReadMore . 2013-08-16 .
  6. Web site: Pioneer Venus Project Information . NASA Goddard Space Flight Center . 2016-08-17 .
  7. Web site: PVO Mission Document . NASA.
  8. Web site: Pioneer Venus Observations during Comet Halley's Inferior Conjunction . C.T. . Russell . J.G. . Luhmann . F.L. . Scarf . University of California, Los Angeles . 1985 . dead . 2009-02-27 . https://web.archive.org/web/20090227202025/http://www-ssc.igpp.ucla.edu/personnel/russell/papers/pioneerVenus_conjunct.pdf . 2013-08-16 .