Ballistic Range Testing of the Mars Exploration Rover Entry CapsuleResults from a 25 shot ballistic range test of the Mars Exploration Rover (MER) aeroshell are presented. The supersonic pitch damping properties of the MER capsule were characterized between Mach = 1.5 and Mach = 3.5 and total angles-of-attack from 0 degrees to greater than 25 degrees. Three capsule center-of-gravity positions were tested across this range of conditions, 0.27, 0.30 and 0.33 body diameters aft of the nose. Parameter identification results show that the capsule is dynamically unstable at low angles-of-attack across the Mach numbers tested, with instability increasing with lower speeds. This dynamic instability was seen to increase with aft center-of-gravity movement. The MER outer mold line was very similar to the successful Mars Pathfinder capsule with only minor modifications. Pathfinder relied on Viking forced oscillation data for preflight predictions. The pitch damping data calculated from this test program are shown to more accurately reproduce the measured Path finder flight data.
Document ID
20050041739
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Schoenenberger, Mark (NASA Langley Research Center Hampton, VA, United States)
Hathaway, Wayne (Arrow Tech Associates, Inc. South Burlington, VT, United States)
Yates, Leslie (Aerospace Computing, Inc. Mountain View, CA, United States)
Desai, Prasun (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 6, 2005
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
AIAA Paper 2005-0055Report Number: AIAA Paper 2005-0055
Meeting Information
Meeting: 43rd AIAA Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 10, 2005
End Date: January 13, 2005
Sponsors: American Inst. of Aeronautics and Astronautics