The mars 2001 ballon design

AIAA International Balloon Technology Conference, 1997

Volumn , Issue , 1997, Pages

  Steve Smith, I ^a   Simpson, Joel M ^a   Raque, Steven M ^a   Said, Magdi A ^a   Cathey, Henry M ^b  

^a NASA GODDARD SPACE FLIGHT CENTER   (United States)

^b NEW MEXICO STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BALLOONS; DESIGN; ENVIRONMENTAL TECHNOLOGY; INDUSTRIAL RESEARCH; NASA; SPACE PLATFORMS; SPACECRAFT; SYSTEMS ANALYSIS; VEHICLE PERFORMANCE;

AMES RESEARCH CENTERS; DESIGN APPROACHES; FRENCH SPACE AGENCY; INDUSTRIAL PARTNERS; JET PROPULSION LABORATORY; LOCKHEED MARTIN AERONAUTICS; NASA GODDARD SPACE FLIGHT CENTER; SPACE DYNAMICS LABORATORIES;

SPACE FLIGHT;

EID: 84977083723     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1997-1448     Document Type: Conference Paper

References (8)

1. Tarrieu, C, "Status of the Mars 96 Aerostat Development" IAF paper, Graz, Austria, October 1993.
2. Greeley, R., et al., "The Mars Aerial Platform Mission Concept", AIAA paper 96-0335, 34th Aerospace Sciences Meeting, Reno, NV, January 1996.
3. Nock, K.T., J. Balaram, M. K. Heun, I. S. Smith, T. Camber, "Mars 2001 Aerobot/Balloon System Overview", AIAA International Balloon Technology Conference, San Francisco, California, 3-5 June 1997.
4. Lally, V.T., "The Radiation Controlled Balloon (RACOON)", Adv. Space Res. Vol. 3, No. 6, pp. 19-24,1983.
5. Simpson, J.M., "Overpressurized Zero Pressure Balloon System",AIAA-91-3671-CP
6. Heun, M. K., H. M. Cathey Jr., R. Haberle, "Mars Balloon Trajectory Model for Mars Geoscience Aerobot Development", AIAA International Balloon Technology Conference, San Francisco, California, 3-5 June 1997.
7. Lally, V.T., "Superpressure Balloons for Horizontal Soundings of the Atmosphere", NCAR-TN-28, 1967.
8. Frykman, R. W., Johnson, P.H., Schumann, A.P., Stenlund, S.J., "Carrier Balloon Test Flights from Oakey, Australia January 1973, NCAR-TN/STR-97,1974