An Evaluation of Ballute Entry Systems for Lunar Return Missions

Author:

Clark Ian1,Braun Robert1,Theisinger John1,Wells Grant1

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Reference21 articles.

1. Miller, K. L., Gulick, D., Lewis, J., Trochman, B., Stein, J., Lyons, D. T., and Wilmoth, R. G. "Trailng Ballute Aerocapture: Concept and FeasibilityAssessment," AIAAPaper 2003-4655,July2003.

2. Assessment of Aerocapture Flight at Titan Using a Drag-Only Device

3. Graesslin,M.,andSchoettle,U."FlightPerformanceEvaluationoftheRe-EntryMissionIRDT-1,"PaperIAF-01-V.3.05,52ndInternationalAstronauticalCongress,Toulouse,France,Oct.1-52001.

4. Inflatable Re-entry Vehicle Experiment (IRVE) Design Overview

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3. Ultra Lightweight Ballutes for Return to Earth from Moon;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05

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