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Comet rendezvousA Mariner Mark II spacecraft rendezvous mission with comet Kopff has been recommended by NASA's Solar System Exploration Committee, and is scheduled for a Shuttle launch in 1990. The spacecraft, which is scheduled to encounter the comet in 1994, will conduct a series of experiments including the study of the cometary nucleus, coma, and tail during perihelion passage; the determination of the nucleus and coma chemical/isotropic composition; the description of the nucleus's size, mass, rotation period, and pole occultation; distinctions of gas and dust hydrodynamics; and distinctions of solar wind interactions with the coma. The three-axis-stabilized spacecraft will be modular in design, and will incorporate a 490-Newton Insat engine, Viking Orbiter propulsion tanks, an Integrated Platform Pointing and Attitude Control Subsystem, and several scientific instruments. The spacecraft's Radio Frequency Subsystem will only use X-band telemetry with a downlink frequency of 8415 MHz, and an uplink frequency of 7161 MHz. The power sources in the present design include one radioisotope thermoelectric generator, three 3 Ah batteries, and a solar panel of approximately 7 sq m.
Document ID
19840061782
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Draper, R. F.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lundy, S. A.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Date Acquired
August 12, 2013
Publication Date
August 1, 1984
Publication Information
Volume: 37
ISSN: 0007-084X
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
ISSN: 0007-084X
Accession Number
84A44569
Distribution Limits
Public
Copyright
Other

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