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The Mars Exploration Rover (MER) Transverse Impulse Rocket System (TIRS)In a very short period of time the MER project successfully developed and tested a system, TIRS/DIMES, to improve the probability of success in the presence of large Martian winds. The successful development of TIRS/DIMES played a big role in the landing site selection process by enabling the landing of Spirit on Gusev crater, a site of very high scientific interest but with known high wind conditions. The performance of TIRS by Spirit at Gusev Crater was excellent. The velocity prediction error was small and Big TIRS was fired reducing the impact horizontal velocity from approximately 23 meters per second to approximately 11 meters per second, well within the airbag capabilities. The performance of TIRS by Opportunity at Meridiani was good. The velocity prediction error was rather large (approximately 6 meters per second, a less than 2 sigma value, but TIRS did not fire which was the correct action.
Document ID
20090014205
Acquisition Source
Jet Propulsion Laboratory
Document Type
Presentation
External Source(s)
Authors
SanMartin, Alejandro Miguel
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bailey, Erik
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 24, 2013
Publication Date
February 10, 2005
Subject Category
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: Guidance and Control Conference
Location: Breckenridge, CO
Country: United States
Start Date: February 10, 2005
Distribution Limits
Public
Copyright
Other
Keywords
Transverse Impulse Rocket System (TIRS)
Entry, Descent, Landing (EDL)
Mars Exploration Rover

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