NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Drogue Parachute Effects on the Orion Crew Module StabilityA forced oscillation test of the Orion Crew Module (CM) was conducted in the Langley 20-Foot Vertical Spin Tunnel. The objective of the test was to quantify the rate damping characteristics of the CM-drogue chute system. Numerous configurations were tested to measure the influence of the chutes on the CM dynamic aerodynamics and, conversely, the influence of the CM on drogue performance. Results show that the CM-drogue system is well-damped at all combinations of frequency, amplitude, and Strouhal number. The wake of the CM significantly reduces the drogue chute riser line force, and the drogues have little upstream influence on the CM aerodynamics. These results are being used to improve simulation model fidelity of CM flight with drogues deployed, which has been identified by the project as key to a successful Orion Critical Design Review.
Document ID
20110013284
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Aubuchon, Vanessa V.
(NASA Langley Research Center Hampton, VA, United States)
Owens, D. Bruce
(NASA Langley Research Center Hampton, VA, United States)
Fremaux, C. Michael
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
June 27, 2011
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA-2011-3505
NF1676L-11685
Report Number: AIAA-2011-3505
Report Number: NF1676L-11685
Meeting Information
Meeting: 29th AIAA Applied Aerodynamics Conference
Location: Honolulu, HI
Country: United States
Start Date: June 27, 2011
End Date: June 30, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 644423.06.31.03.15.04.20
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available