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Flight path control strategies and preliminary deltaV requirements for the 2007 Mars Phoenix (PHX) missionThis paper describes the methods used to estimate the statistical deltaV requirements for the propulsive maneuvers that will deliver the spacecraft to its target landing site while satisfying planetary protection requirements. the paper presents flight path control analysis results for three different trajectories, open, middle, and close of launch period for the mission.
Document ID
20060042922
Document Type
Conference Paper
External Source(s)
Authors
Raofi, Behzad
Date Acquired
August 23, 2013
Publication Date
August 1, 2005
Subject Category
Lunar and Planetary Science and Exploration
Meeting Information
AAS/AIAA Astrodynamics Specialist Conference(Lake Tahoe, CA)
Distribution Limits
Public
Copyright
Other
Keywords
Phoenix
maneuver
deltaV
Mars
TCM