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Development and Testing of a Drogue Parachute System for X-37 ALTV/B-52H SeparationMultiple scenarios were identified in which the X-37 approach and landing test vehicle (ALTV) catastrophically recontacts the B-52H carrier aircraft after separation. The most cost-effective recontact risk mitigation is the prelaunch deployment of a drogue parachute that is released after the X-37 ALTV has safely cleared the B-52H. After release, a fully-inflated drogue parachute takes 30 min to reach ground and results in a large footprint that excessively restricts the days available for flight. To reduce the footprint, a passive collapse mechanism consisting of an elastic reefing line attached to the parachute skirt was developed. At flight loads the elastic is stretched, allowing full parachute inflation. After release, drag loads drop dramatically and the elastic line contracts, reducing the frontal drag area. A 50-percent drag reduction results in an approximately 75-percent ground footprint reduction. Eleven individual parachute designs were evaluated at flight load dynamic pressures in the High Velocity Airflow System (HIVAS) at the Naval Air Warfare Center (NAWC), China Lake, California. Various options for the elastic reefing system were also evaluated at HIVAS. Two best parachute designs were selected from HIVAS to be carried forward to flight test. Detailed HIVAS test results are presented in this report.
Document ID
20040066087
Acquisition Source
Armstrong Flight Research Center
Document Type
Technical Memorandum (TM)
Authors
Whitmore, Stephen A.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Cobleigh, Brent R.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Jacobson, Steven R.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Jensen, Steven C.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Hennings, Elsa J.
(Naval Air Warfare Center China Lake, CA, United States)
Date Acquired
September 7, 2013
Publication Date
May 1, 2004
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2004-212044
H-2552
Report Number: NASA/TM-2004-212044
Report Number: H-2552
Meeting Information
Meeting: 42nd AIAA Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 5, 2004
End Date: January 8, 2004
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WORK_UNIT: WU 760-90-00-SE-53-00-37A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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