Title:
Aerobraking Cost/Risk Decisions
Aerobraking Cost/Risk Decisions
Author(s)
Spencer, David A.
Tolson, Robert
Tolson, Robert
Advisor(s)
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Abstract
Three missions have successfully used aerobraking to reduce the spacecraft orbit period
and achieve the desired orbit geometry. A fourth, Mars Reconnaissance Orbiter, will
employ aerobraking following its orbit insertion in March, 2006. The propellant mass
reductions enabled by the aerobraking technique allow the use of smaller launch systems,
which translate to significant savings in launch costs for flight projects. However, there is
a significant increase in mission risk associated with the use of aerobraking. Flying a
spacecraft through a planetary atmosphere hundreds of times during months of aroundthe-
clock operations places the spacecraft in harm’s way, and is extraordinarily
demanding on the flight team. There is a cost/risk trade that must be evaluated when a
project is choosing between a mission baseline that includes aerobraking, or selecting a
larger launch vehicle to enable purely propulsive orbit insertion. This paper provides a
brief history of past and future aerobraking missions, describes the aerobraking
technique, summarizes the costs associated with aerobraking, and concludes with a
suggested methodology for evaluating the cost/risk trade when selecting the aerobraking
approach.
Sponsor
AIAA Space Systems Technical Committee ; AIAA Space Transportation Systems Technical Committee ; Space Technology Advanced Research Center
Date Issued
2005-11-10
Extent
429705 bytes
1558270 bytes
1905 bytes
429705 bytes
1558270 bytes
1558270 bytes
1905 bytes
429705 bytes
1558270 bytes
Resource Type
Text
Resource Subtype
Presentation