Design and development of the main parachute for the beagle 2 Mars lander

17th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar

Volumn , Issue , 2003, Pages

  Fallon II, Edward J ^a   Sinclair, Robert ^a  

^a Irvin Aerospace Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894688149     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (21)

1. Fallon II, Edward J.; System Design Overview of the Mars Pathfinder Parachute Decelerator Subsystem; AIAA paper no. 97-1511; 14th AIAA Aerodynamic Decelerator Systems Technology Conference; June 1997.
2. Steinberg, S., Siemers, P., and Slayman, R.; Development of the Viking Parachute Configuration by Wind Tunnel Investigation; AIAA 4th Aerodynamic Deceleration Systems Conference; AIAA paper no. 73-454; Palm Springs, CA; 21-23 May 1973.
3. Corridan, R., Givens, J., and Kepley, B.; Transonic Wind Tunnel Investigation of the Galileo Probe Parachute Configuration; AIAA 8th Aerodynamic Decelerator and Balloon Technology Conference; AIAA paper no. 84-0823; Hyannis, MA; 2-4 April 1984.
4. Lingard, J. and Underwood, J.; Wind Tunnel Testing of Disk-Gap-Band Parachutes Related to the Cassini-Huygens Mission; RaeS/AIAA 12th Aerodynamic Decelerator Systems Technology Conference and Seminar; AIAA paper no. 98-1200; London, UK; 10-13 May 1993.
5. Campbell, J. F. and Brown Jr., C. A.; Evaluation of Experimental Flow Properties in the Wake of a Viking '75 Entry Vehicle; AIAA paper no. 73-475; AIAA 4th Aerodynamic Deceleration Systems Conference; Pal Springs, CA; May 1973.
6. Preisser, J. C. and Greene, G. C.; Effect of Suspension Line Elasticity on Parachute Loads; Journal of Spacecraft and Rockets, vol. 7 no. 10, pp. 1278-1280; October 1970.
7. Jacobsen, L. S. and Ayre, R. S.; Engineering Vibrations, Chap. 4; McGraw-Hill; New York; 1958.
8. Ewing, E. G., Bixby, H. W., and Knacke, T. W.; Recovery Systems Design Guide; AFFDL-TR-78- 151; Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base, Ohio; June 1978; pp. 336-337.
9. Lingard, J. S., Underwood, J. C.; The Effects of Low Density Atmosphere on the Aerodynamic Coefficients of Parachutes; 13th Aerodynamic Decelerator Systems Technology Conference; AIAA paper no. 95-1556; May 1995.
10. Lingard, J. S., Underwood, J. C.; The Effects of Low Density Atmosphere on the Aerodynamic Coefficients of Parachutes; 13th Aerodynamic Decelerator Systems Technology Conference; AIAA paper no. 95-1556; May 1995.
11. Heinrich, H. G. and Haak, E. L.; Stability and Drag of Parachutes with Varying Effective Porosity; ASD-TDR-62-100; Aeronautical Systems Division; Wright-Patterson AFB; September 1962.
12. Payne, P. R.; The Theory of Parachute Fabric Porosity as Applied to Parachutes in Incompressible Flow; The Aeronautical Quarterly, vol. 29; August 1978.
13. Fallon II, Edward J.; System Design Overview of the Mars Pathfinder Parachute Decelerator Subsystem; AIAA paper no. 97-1511; 14th AIAA Aerodynamic Decelerator Systems Technology Conference; June 1997.
14. Ewing, E.G., Bixby, H.W., and Knacke, T.W.; Recovery Systems Design Guide; AFFDL-TR-78- 151; Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base, Ohio; June 1978; pp. 299.
15. Ewing, E.G., Bixby, H.W., and Knacke, T.W.; Recovery Systems Design Guide; AFFDL-TR-78- 151; Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base, Ohio; June 1978; pp. 299.
16. Gionfrido, Maurice Paul.; A Method for Determining Airdrop System Characteristics for Minimum Altitude Loss to Equilibrium; Master Thesis; Massachusetts Institute of Technology; January, 1969.
17. Gionfrido, Maurice Paul.; A Method for Determining Airdrop System Characteristics for Minimum Altitude Loss to Equilibrium; Master Thesis; Massachusetts Institute of Technology; January, 1969.
18. Delurgio, P. R. and North, R. N.; Parametric Analysis and Design Considerations for Mars Parachute Landing System; TP 121; AIAA Aerodynamic Deceleration Systems Conference; Houston, TX; September 1966.
19. Delurgio, P. R. and North, R. N.; Parametric Analysis and Design Considerations for Mars Parachute Landing System; TP 121; AIAA Aerodynamic Deceleration Systems Conference; Houston, TX; September 1966.
20. Ewing, E. G.; Technical Justification for Two Advanced Design Principles Recommended for Ringsail Parachutes; Memo; 1971.
21. Delurgio, Phillip R.; Evolution of the Ringsail Parachute; AIAA paper no. 99-1700; 15th CEAS/AIAA Aerodynamic Decelerator Systems Technology Conference; June 1999.