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High Pressure Earth Storable Rocket Technology Program-Hipes Options 1/2 Report
| AUTHOR | Nasa, National Aeronautics and Space Adm |
| PUBLISHER | Independently Published (09/19/2018) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
Under the High Pressure Earth Storable Rocket Technology (HIPES) Program, TRW successfully completed testing of two 100 lbf thrust class rhenium chambers using N204-MMH. The first chamber was successfully fired for 4789 seconds of operating time with a maximum duration of 700 seconds. This chamber had been previously fired for 5230 seconds with N2O4-N2H4. The second chamber was successfully fired for 8085 seconds with a maximum firing duration of 1200 seconds. The Isp (specific impulse) for both chambers ranged from 323 lbf-sec/lbm to 330 lbf-sec/lbm.Chazen, M. L. and Sicher, D. and Calvignac, J. and Ono, D.Glenn Research CenterHIGH PRESSURE; THRUST CHAMBERS; ROCKET ENGINE DESIGN; ENGINE TESTS; SPACE STORAGE; METHYLHYDRAZINE; RHENIUM; PINTLES; INJECTORS; SPECIFIC IMPULSE; TEST FIRING...
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Product Format
Product Details
ISBN-13:
9781723849084
ISBN-10:
1723849081
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
More Product Details
Page Count:
58
Carton Quantity:
70
Product Dimensions:
8.50 x 0.12 x 11.02 inches
Weight:
0.35 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Science | Space Science - General
Descriptions, Reviews, Etc.
publisher marketing
Under the High Pressure Earth Storable Rocket Technology (HIPES) Program, TRW successfully completed testing of two 100 lbf thrust class rhenium chambers using N204-MMH. The first chamber was successfully fired for 4789 seconds of operating time with a maximum duration of 700 seconds. This chamber had been previously fired for 5230 seconds with N2O4-N2H4. The second chamber was successfully fired for 8085 seconds with a maximum firing duration of 1200 seconds. The Isp (specific impulse) for both chambers ranged from 323 lbf-sec/lbm to 330 lbf-sec/lbm.Chazen, M. L. and Sicher, D. and Calvignac, J. and Ono, D.Glenn Research CenterHIGH PRESSURE; THRUST CHAMBERS; ROCKET ENGINE DESIGN; ENGINE TESTS; SPACE STORAGE; METHYLHYDRAZINE; RHENIUM; PINTLES; INJECTORS; SPECIFIC IMPULSE; TEST FIRING...
Show More