A viewgraph presentation on the design of a lightweight non-intrusive force measurement device (FMD) to reduce the cost per effective payload (PL) mass into orbit (CPMO) by improving launch vehicle (LV) loads and environments.
Flight Loads and Environments Initiative
2005 Spacecraft and Launch Vehicle Dynamic Environments Workshop ; 2005 ; Los Angeles, CA, United States
2005-01-01
Preprint
No indication
English
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