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Mars Smart Lander Parachute Simulation ModelA multi-body flight simulation for the Mars Smart Lander has been developed that includes six degree-of-freedom rigid-body models for both the supersonically-deployed and subsonically-deployed parachutes. This simulation is designed to be incorporated into a larger simulation of the entire entry, descent and landing (EDL) sequence. The complete end-to-end simulation will provide attitude history predictions of all bodies throughout the flight as well as loads on each of the connecting lines. Other issues such as recontact with jettisoned elements (heat shield, back shield, parachute mortar covers, etc.), design of parachute and attachment points, and desirable line properties can also be addressed readily using this simulation.
Document ID
20030000829
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Queen, Eric M.
(NASA Langley Research Center Hampton, VA United States)
Raiszadeh, Ben
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
AIAA Paper 2002-4617
Report Number: AIAA Paper 2002-4617
Meeting Information
Meeting: AIAA Atmospheric Flight Mechanics Conference and Exhibit
Location: Monterey, CA
Country: United States
Start Date: August 5, 2002
End Date: August 8, 2002
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available