Space shuttle rbar pitch maneuver for thermal protection system inspection

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

Volumn 2, Issue , 2005, Pages 1513-1526

  Walker, Stephen R ^a,d,e   LoPresti, Jessica A ^b,f   Schreck, Mark B ^b,f   Hall, Robert A ^c,f  

^a NASA JOHNSON SPACE CENTER   (United States)

^b United Space Alliance   (United States)

^c CHARLES STARK DRAPER LABORATORY   (United States)

^d Flight Design and Dynamics Division / DM34   (United States)

^e AIAA   (United States)

^f USH 483L ^*

Author keywords

[No Author keywords available]

Indexed keywords

GEOMETRY CONSTRAINTS; INSPECTION PHOTOGRAPHY; RBAR PITCH MANOEUVER (RPM); THERMAL PROTECTION SYSTEM;

DEBRIS; ORBITS; PHOTOGRAPHY; PROPELLANTS; SENSORS; SPACE STATIONS;

SPACE SHUTTLES;

EID: 29744454195     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. Columbia Accident Investigation Board Report Volume 1, August 2003
2. Space Shuttle Operational Groundrules and Constraints Level B, NASA NSTS 21075, November 1998
3. Goodman, J. L., "A GPS Receiver Upgrade For The Space Shuttle - Rationale And Considerations," 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA, Reston, VA, 2004.
4. Hughes, P. C., Spacecraft Attitude Dynamics, John Wiley and Sons, New York, 1986, Chapter 4