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Manned Mars lander launch-to-rendezvous analysis for a 1981 Venus-Swingby mission

Author: Nickolas L Faust; Thomas B Murtagh; United States. National Aeronautics and Space Administration.; Manned Spacecraft Center (U.S.)
Publisher: Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971.
Series: NASA technical note, D-6555.
Edition/Format:   Print book : National government publication : EnglishView all editions and formats
Summary:
A description is given of the return of a manned Mars lander by a launch from the surface of Mars to some intermediate orbit, with subsequent maneuvers to rendezvous with a primary spacecraft (called the orbiter) in a Mars parking orbit. The type of Mars mission used to demonstrate the analytical technique includes a Venus swingby on the Mars-to-Earth portion of the trajectory in order to reduce the total mission  Read more...
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Details

Material Type: Government publication, National government publication, Internet resource
Document Type: Book, Internet Resource
All Authors / Contributors: Nickolas L Faust; Thomas B Murtagh; United States. National Aeronautics and Space Administration.; Manned Spacecraft Center (U.S.)
OCLC Number: 61730498
Description: 21 pages : illustrations ; 27 cm.
Series Title: NASA technical note, D-6555.
Other Titles: NASA TN D-6555
Responsibility: Nickolas L. Faust and Thomas B. Murtagh.

Abstract:

A description is given of the return of a manned Mars lander by a launch from the surface of Mars to some intermediate orbit, with subsequent maneuvers to rendezvous with a primary spacecraft (called the orbiter) in a Mars parking orbit. The type of Mars mission used to demonstrate the analytical technique includes a Venus swingby on the Mars-to-Earth portion of the trajectory in order to reduce the total mission velocity requirement. The total velocity requirement for the mission considered (if inplane launches are assumed) is approximately 17,500 ft/sec.

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Primary Entity

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