| U.S. ROCKETS 38mm MOTOR DETAIL |
38mm 181 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: 161H56.5-P-RSRM Commonly referred to as "H90 Nozzleless". |
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