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Trade Study of Multiple Thruster Options for the Mars Airplane Concept
| AUTHOR | Administration (Nasa), National Aeronaut |
| PUBLISHER | Independently Published (08/21/2020) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
A trade study was performed at NASA Langley Research Center under the Planetary Airplane Risk Reduction (PARR) project (2004-2005) to examine the option of using multiple, smaller thrusters in place of a single large thruster on the Mars airplane concept with the goal to reduce overall cost, schedule, and technical risk. The 5-lbf (22N) thruster is a common reaction control thruster on many satellites. Thousands of these types of thrusters have been built and flown on numerous programs, including MILSTAR and Intelsat VI. This study has examined the use of three 22N thrusters for the Mars airplane propulsion system and compared the results to those of the baseline single thruster system. Kuhl, Christopher A. and Gayle, Steven W. and Hunter, Craig A. and Kenney, Patrick S. and Scola, Salvatore and Paddock, David A. and Wright, Henry S. and Gasbarre, Joseph F. Langley Research Center NASA/TM-2009-215699, L-19371, LF99-5349 WBS 698671.02.07.02.01
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Product Format
Product Details
ISBN-13:
9798676266288
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
More Product Details
Page Count:
78
Carton Quantity:
52
Product Dimensions:
8.50 x 0.16 x 11.02 inches
Weight:
0.45 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Reference | Research
Reference | Space Science - General
Descriptions, Reviews, Etc.
publisher marketing
A trade study was performed at NASA Langley Research Center under the Planetary Airplane Risk Reduction (PARR) project (2004-2005) to examine the option of using multiple, smaller thrusters in place of a single large thruster on the Mars airplane concept with the goal to reduce overall cost, schedule, and technical risk. The 5-lbf (22N) thruster is a common reaction control thruster on many satellites. Thousands of these types of thrusters have been built and flown on numerous programs, including MILSTAR and Intelsat VI. This study has examined the use of three 22N thrusters for the Mars airplane propulsion system and compared the results to those of the baseline single thruster system. Kuhl, Christopher A. and Gayle, Steven W. and Hunter, Craig A. and Kenney, Patrick S. and Scola, Salvatore and Paddock, David A. and Wright, Henry S. and Gasbarre, Joseph F. Langley Research Center NASA/TM-2009-215699, L-19371, LF99-5349 WBS 698671.02.07.02.01
Show More