Crew exploration vehicle ascent abort trajectory analysis and optimization

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2007

Volumn 4, Issue , 2007, Pages 4255-4261

  Falck, Robert D ^a,b,c   Gefert, Leon P ^a,b,c  

^a NASA GLENN RESEARCH CENTER   (United States)

^b Service Module GN and C

^c Space Propulsion and Mission Analysis Office/DDB ^*

Author keywords

[No Author keywords available]

Indexed keywords

ABORT TRAJECTORY ANALYSIS; CREW EXPLORATION VEHICLES; CREW SURVIVABILITY;

MANNED SPACE FLIGHT; NASA; SPACE SHUTTLES; SPACE STATIONS; SPACECRAFT PROPULSION;

TRAJECTORIES;

EID: 37349128310     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Constellation Architecture Requirements Document, CxP 70000, 16 Aug. 2006.
2. Henderson, E. M. and Butler, J. V., "Spacecraft Operational Abort Plan for Apollo 7 (Mission C). Volume 2: CSM Launch Aborts," NASA TM 69694, 19 July, 1968.
3. Riehl, J. P., Paris, S. W., and Sjauw, W. K., "Comparison of Implicit Integration Methods for Solving Aerospace Trajectory Optimization Problems," AIAA 2006-6033, 21-24 Aug. 2006.
4. Falck, R. D., Burke, L. M., and Gefert, L. P., "CEV RAC-2 TDS-04-012/Subtask 5: Late Ascent Abort Modeling Sensitivities Analysis," NASA FltDyn-CEV-06-92, 11 Sept. 2006.