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. The spacecraft conducted radar altimetry observations allowing the first global topographic map of the Venusian surface to be constructed.
Spacecraft
Manufactured by Hughes Aircraft Company, the Pioneer Venus Orbiter was based on the HS-507 bus. 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.
Instruments The Pioneer Venus Orbiter carried 17 experiments with a total mass of 45 kilograms (99 lb):
Orbiter Cloud Photopolarimeter (OCPP) The Orbiter Cloud Photopolarimeter was used to measure the vertical distribution of clouds on Venus. It was a photo-polarimeter built by the Goddard Institute for Space Studies (GISS), similar to Pioneer 10 and Pioneer 11 imaging photopolarimeter (IPP), and operating on four spectral bands (255-285, 355-380, 540-555, and 930-945 nm). The principal investigator was J. Hansen, later succeeded by L. Travis. The instrument had a mass of 5 kilograms and consumed 5.4 watts of power.
Orbiter Radar Mapper Instrument (ORAD) The Orbiter Radar Mapper Instrument was designed to determine the topography and surface characteristics of Venus. It was a radar system developed by the Massachusetts Institute of Technology (MIT), with G. Pettengill serving as the principal investigator. Weighing 9 kilograms and consuming 18 watts, the instrument operated when the spacecraft was within 4,700 kilometres (2,900 mi) of the planet. It transmitted a 20-watt S-band signal at 1.757 Gigahertz and achieved a surface mapping resolution of 23 by 7 kilometres (14.3 mi × 4.3 mi) at periapsis.
Orbiter Infrared Radiometer (OIR) The Orbiter Infrared Radiometer was used to measure infrared emissions from Venus's atmosphere. It was constructed by the Jet Propulsion Laboratory (JPL), and the principal investigator was F. Taylor. The instrument had a mass of 5.9 kilograms and required 5.2 watts of power.
Orbiter Ultraviolet Spectrometer (OUVS) The Orbiter Ultraviolet Spectrometer measured scattered and emitted ultraviolet light from Venus. Built by the Laboratory for Atmospheric and Space Physics (LASP), its principal investigator was A.I.F. Stewart. The spectrometer weighed 3.1 kilograms and consumed 1.7 watts of power.
Orbiter Neutral Mass Spectrometer (ONMS)
The Orbiter Neutral Mass Spectrometer was used to determine the composition of Venus's upper atmosphere. Manufactured by the Goddard Space Flight Center (GSFC), it was managed by principal investigator H. Neimann. The instrument had a mass of 3.8 kilograms and consumed 12 watts.
Orbiter Plasma Analyzer (OPA)
The Orbiter Plasma Analyzer measured properties of the solar wind. Developed at the Ames Research Center (ARC), the instrument was led by principal investigator J. Wolfe, who was later succeeded by A. Barnes. It had a mass of 3.9 kilograms and required 5 watts of power.
Orbiter Magnetometer (OMAG) The Orbiter Magnetometer was designed to characterize Venus’s magnetic field. It was built by the University of California, Los Angeles (UCLA), with C. Russell as the principal investigator. The 2-kilogram instrument consumed 2.2 watts of power and was mounted on a 4.7-meter boom to reduce spacecraft interference.
Orbiter Electric Field Detector (OEFD)
The Orbiter Electric Field Detector studied electric fields in the Venusian environment. Built by TRW and led by principal investigator F. Scarf, it had a mass of 0.8 kilograms and used only 0.7 watts of power.
Orbiter Electron Temperature Probe (OETP)
The Orbiter Electron Temperature Probe investigated the thermal properties of Venus’s ionosphere. It was developed by the Goddard Space Flight Center (GSFC) under the direction of principal investigator L. Brace. The probe had a mass of 2.2 kilograms and consumed 4.8 watts.
Orbiter Ion Mass Spectrometer (OIMS)
The Orbiter Ion Mass Spectrometer was used to characterize the ion population in the ionosphere of Venus. Built by the Goddard Space Flight Center (GSFC), it was managed by principal investigator H. Taylor. The instrument had a mass of 3 kilograms and required 1.5 watts of power.
Orbiter Retarding Potential Analyzer (ORPA) The Orbiter Retarding Potential Analyzer studied ionospheric particles. It was developed at the Lockheed Palo Alto Research Laboratory (LPARL), with W. Knudsen as the principal investigator. This instrument weighed 2.8 kilograms and consumed 2.4 watts of power.
Orbiter Gamma-Ray Burst Detector (OGBD) The Orbiter Gamma-Ray Burst Detector recorded gamma-ray burst events. It was constructed by the Los Alamos Scientific Laboratory (LASL), and W. Evans served as the principal investigator. The instrument had a mass of 2.8 kilograms.
Experiments The orbiter also performed in situ radio science experiments:
Orbiter Atmospheric Propagation Experiment (OGPE) The OGPE utilized dual-frequency radio signals to investigate how Venus's atmosphere affects radio wave propagation. By analyzing signal attenuation and phase shifts, the experiment aimed to deduce atmospheric properties such as electron density and refractive index. This information is crucial for understanding the structure and composition of Venus's ionosphere. T. Croft from SRI was the principal investigator.
Orbiter Atmospheric Drag Experiment (OAD) The OAD measured the deceleration of the spacecraft due to atmospheric drag at the fringes of Venus's atmosphere. By tracking changes in the spacecraft's velocity, the experiment provided data on atmospheric density and its variations with altitude and solar activity. G. Keating from LRC was the principal investigator.
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