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SPRITE: A TPS Test Bed for Ground and FlightEngineers in the Entry Systems and Technology Division at NASA Ames Research Center developed a fully instrumented, small atmospheric entry probe called SPRITE (Small Probe Reentry Investigation for TPS Engineering). SPRITE, conceived as a flight test bed for thermal protection materials, was tested at full scale in an arc-jet facility so that the aerothermal environments the probe experiences over portions of its flight trajectory and in the arc-jet are similar. This ground-to-flight traceability enhances the ability of mission designers to evaluate margins needed in the design of thermal protection systems (TPS) of larger scale atmospheric entry vehicles. SPRITE is a 14-inch diameter, 45 deg. sphere-cone with a conical aftbody and designed for testing in the NASA Ames Aerodynamic Heating Facility (AHF). The probe is a two-part aluminum shell with PICA (phenolic impregnated carbon ablator) bonded on the forebody and LI-2200 (Shuttle tile material) bonded to the aftbody. Plugs with embedded thermocouples, similar to those installed in the heat shield of the Mars Science Laboratory (MSL), and a number of distributed sensors are integrated into the design. The data from these sensors are fed to an innovative, custom-designed data acquisition system also integrated with the test article. Two identical SPRITE models were built and successfully tested in late 2010-early 2011, and the concept is currently being modified to enable testing of conformable and/or flexible materials.
Document ID
20140008307
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Prabhu, Dinesh K.
(Engineering Research and Consulting, Inc. Mountain View, CA, United States)
Agrawal, Parul
(Engineering Research and Consulting, Inc. Mountain View, CA, United States)
Peterson, Keith
(Engineering Research and Consulting, Inc. Mountain View, CA, United States)
Swanson, Gregory
(Engineering Research and Consulting, Inc. Mountain View, CA, United States)
Skokova, Kristina
(Engineering Research and Consulting, Inc. Mountain View, CA, United States)
Mangini, Nancy
(Engineering Research and Consulting, Inc. Mountain View, CA, United States)
Empey, Daniel M.
(Sierra Lobo, Inc. Moffett Field, CA, United States)
Gorbunov, Sergey
(Sierra Lobo, Inc. Moffett Field, CA, United States)
Venkatapathy, Ethiraj
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
June 16, 2014
Publication Date
February 28, 2012
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN4730
Report Number: ARC-E-DAA-TN4730
Meeting Information
Meeting: AFOSR/NASA/Sandia Ablation Workshop
Location: Lexington, KY
Country: United States
Start Date: February 28, 2012
End Date: March 1, 2012
Sponsors: Sandia Corp., Air Force Office of Scientific Research, NASA
Funding Number(s)
CONTRACT_GRANT: NNA10DE12C
CONTRACT_GRANT: NNA09DB39C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Ablation
Atmospheric entry
Thermal Protection System
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