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Ion propulsion for a Mars sample return missionThis paper describes the an on-going study to examine the feasibility of using SEP based on derivatives of the Deep Space 1 ion propulsion system (IPS) technology to enable a Mars Sample Return (MSR mission to be performed from a single medium-class launch vehicle.
Document ID
20210002573
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/15789
Authors
Rodgers, D. H.
Brophy, J. R.
Date Acquired
July 17, 2000
Publication Date
July 17, 2000
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Mars
sample
return
MSR
ion
propulsion
SEP
ion
engine
solar
electronic
propulsion

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