Lunar lander configuration study and parametric performance analysis

Author:

DONAHUE BENJAMIN1,FOWLER C.1

Affiliation:

1. Boeing Defense & Space Group, Huntsville, AL

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. FourthQuarterlyReview. SpseTransferConceptsandAnalysisforExplorationMissions wnuacf (WCAeM),NAS8-37857. AdvancedCivilSpaceSystems(Hunwvillc.Al).BocingDefcnse&SpaceGroup.Oct 1990

2. ResearchandDevebpmenlSlralegyforbfiningandProcersing inSpace.BurenuofMincs.Ckt 1990

3. InterimReviewBriqingNo.1, SpaceTrwsferVehicleConceptsandRequirementsStudy.NAS8-37856.MartinMraiew Dec 1990

4. S IntuimRevimBriqingNo.3. SpseTransferVehiflcCandReSmdy.NAS8-37855.BoeingDefame&SpaceGroup(Seattle).June 1990

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1. Lunar Lander Concepts for Human Exploration;Journal of Spacecraft and Rockets;2008-03

2. Lunar Lander Concept Design for the 2019 NASA Outpost Mission;AIAA SPACE 2007 Conference & Exposition;2007-06-18

3. Human Mars missions - Cost driven architecture assessments;AIAA Defense and Civil Space Programs Conference and Exhibit;1998-08-22

4. Mars ascent concept using NTR with lithium propellant;34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;1998-07-13

5. Calculation of Pitch Damping for a Flared Projectile;Journal of Spacecraft and Rockets;1997-07

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