Genesis mission design

AIAA/AAS Astrodynamics Specialist Conference and Exhibit

Volumn , Issue , 1998, Pages 1-12

  Lo, Martin W ^a   Williams, Bobby G ^a   Bollman, Williard E ^a   Han, Dongsuk ^a   Hahn, Yungsun ^a   Bell, Julia L ^a   Hirst, Edward A ^a   Corwin, Robert A ^b   Hong, Philip E ^b   Howell, Kathleen C ^c   Barden, Brian ^c   Wilson, Roby ^c  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^b LOCKHEED MARTIN   (United States)

^c PURDUE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASTROPHYSICS; SOLAR SYSTEM; SOLAR WIND;

GENESIS MISSION; GENESIS SPACECRAFT; HALO ORBITS; SOLAR WIND SAMPLES; ULTRAPURE MATERIALS;

ORBITS;

EID: 84983097781     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. Rapp, D., et al, The Suess-Urey Mission, Acta Astronautica V. 39, No. 1-4, 1996, 229-238
2. Gomez, G., Llibre, J., Martinez, R., Simo, C., Station Keeping of Libration Point Orbits, Final Report, Nov. 1985, ESA Contract Report, ESCO Contract No. 5648/83/D/JS (SC)
3. Jordan, P., SOHO Mission Description and Flight Dynamics Analysis Reports, Rev. 2, Sept. 1993, GSFC Doc. No. 554-FDD-91/026ROUDO
4. Farquhar, R., Muhonen, D., Richardson, D., Mission Design for a Halo Orbiter of the Earth, J. Spacecraft, V. 14, No. 3, 1977, pp. 170-177
5. Farquhar, R., Muhonen, D., Newman, C., Heuberger, H., The First Libration-Point Satellite: Mission Overview and Flight History, AAS/AIAA Astrodynamics Conference, Provincetown, MA, June, 1979, Paper 79-126
6. Farquhar, R., Muhonen, D., Newman, C., Heuberger, H., Trajectories and Orbital Maneuvers for the First Libration-Point Satellite, J. Guidance and Control, V. 3, No. 6, 1980, pp. 549-554
7. Howell, K., Harden, B., Lo, M., Application of Dynamical Systems Theory to Trajectory Design for a Libration Point Mission, Journal of Astronautical Sciences, V. 45, No. 2, April-June 1997, 161-178
8. Barden, B., Using Stable Manifolds to Generate Transfers in the Circular Restricted Problem of Three Bodies, Master Thesis, Purdue University, December 1994
9. Lo, M., Ross, S., Low Energy Interplanetary Transfers Using the Invariant Manifolds of LI, L2, and Halo Orbits, AAS Astrodynamics Conference, Monterey, CA., Feb. 1998, Paper No. AAS 98-136