Mission design for the lunar reconnaissance orbiter

Advances in the Astronautical Sciences

Volumn 128, Issue , 2007, Pages 421-436

  Beckman, Mark ^a  

^a NASA GODDARD SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

LAUNCH WINDOW; LUNAR POLAR ORBIT; LUNAR RECONNAISSANCE ORBITER; SPACE EXPLORATION;

ENERGY TRANSFER; NASA; RECONNAISSANCE AIRCRAFT;

LUNAR MISSIONS;

EID: 38549133439     PISSN: 00653438     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. K. Richon & L. Newman, "Flight dynamics support for the Clementine Deep Space Program Science Experiment (DSPSE) mission", AAS/AIAA Astrodynamics Conference, Halifax, Canada. 1995
2. D. Folta, et. al., "Lunar Prospector Mission: Results of Trajectory Design, Quasi-Frozen Orbits, Extended Mission Targeting, and Luna Topography and Potential Models", AAS99-397, Astrodynamics Specialist Conference, Girdwood, AK. 1999
3. M. Beckman & D. Folta, "Mission Design of the First Robotic Lunar Exploration Program Mission: The Lunar Reconnaissance Orbiter", AAS-05-300, AAS/AIAA Astrodynamics Specialists Conference, Lake Tahoe, CA. 2005
4. M. Houghton, "LRO Mission Requirements Document", 431 -RQMT-000004
5. T. Ely & Lieb, "Constellations of Elliptical Inclined Lunar Orbits Providing Polar and Global Coverage", AAS/AIAA Astrodynamics Specialist Conference, Lake Tahoe, CA. 2005.
6. D. Folta & D. Quinn, "Lunar Frozen Orbits", AAS/AIAA Astrodynamics Specialist Conference, Keystone, CO. 2006.
7. M. Beckman & M. Concha, "Lunar Prospector Orbit Determination Results", AIAA-98-4561, Astrodynamics Specialist Conference, Boston, MA. 1998
8. E. Carranza, et. al., "Lunar Prospector Orbit Determination Uncertainties Using the High Resolution Lunar Gravity Models", AAS-99-325, Astrodynamics Specialists Conference, Girdwood, AK. 1999