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Mars Aerobot MicromissionThe Mars Aerobot Micromission is almost a factor of 10 smaller than earlier concepts for a Mars balloon. A key goal is to achieve high payload mass fraction in a small total systems mass and to maximize the scientific potential of that payload. Scientific objectives include studies of the surface with a high resolution stereo imaging magnetometer and investigations of the structure and dynamics of the atmosphere with an in situ meteorology payload.
Document ID
20000052461
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
Authors
Greeley, Ronald (Arizona State Univ. Tempe, AZ United States)
Cutts, James A. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Arvidson, Raymond (Washington Univ. Saint Louis, MO United States)
Blamont, Jacques (Centre National d'Etudes Spatiales Paris, France)
Blaney, Diana L. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Cameron, Jonathon (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Kerzhanovich, Viktor (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Smith, I. Steve (NASA Wallops Flight Facility Wallops Island, VA United States)
Yavrouian, Andre (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: Mars Exploration Programme and Sample Return Missions: Mars Micromissions Workshop
Country: United States
Start Date: February 1, 1999
End Date: February 2, 1999
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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