Revisiting MEDLI with Improved Modeling and Simulation ToolsThe thermal protection system (TPS) of the Mars 2020 capsule will carry a suite of sensors called MEDLI2 (Mars Entry, Descent, and Landing Instrument 2). This suite consists of pressure sensors/transducers and thermocouple plugs meant to measure atmospheric properties, vehicle attitude, TPS performance, etc. While the suite is similar to that carried on the successful MSL (Mars Science Laboratory) mission in 2012, it now includes pressure sensors, thermocouple plugs, and radiometers on the backshell as well. An analysis plan is therefore necessary to help with the interpretation of flight measurements.
Document ID
20210013883
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
D. K. Prabhu (Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
B. A. Cruden (Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
J. D. Monk (Ames Research Center Mountain View, California, United States)
A. P. Borner (Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
J. M. Thornton (Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
J. B. E. Meurisse (Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
April 16, 2021
Subject Category
Lunar And Planetary Science And Exploration
Meeting Information
Meeting: IPPW 2021: 18th International Planetary Probe Workshop
Location: Virtual Event
Country: US
Start Date: June 17, 2021
End Date: August 10, 2021
Sponsors: Analytical Mechanics Associates (United States), University of Glasgow
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Atmospheric EntryHypersonicsThermal Protection SystemEntry Systems and Modeling