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Genesis of LMR & HPR.

U.S. Rockets Nozzleless Motor!

U.S. ROCKETS 38mm MOTOR DETAIL
U.S. ROCKETS
Motor thrust curve graphic
38mm 167.8 H 56.5 -P RSRM

Test data from TRA TMT March 1993.

Total Impulse 37.73 Lb-sec, 167.8 N-s
Average Thrust: 12.70 Lb, 56.52 N
Burn Time: 2.97 Sec
ILP: 168H56.5-P-RSRM

Commonly referred to as "H90 Nozzleless".
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