Apogee | 8000 ft |
Wet Mass at Launch | >450 lbs |
Flight Duration | 40 s |
Burn Duration | 11 s |
MSL Thrust | >1200 lbf |
RP-D2, originally developed by MASA for the TSM program, has been improved and repurposed for the Clementine vehicle. RP-D2 features an inner copper liner, outer aluminum jacket, and a like-doublet injector design. MASA hotfired RP-D2 in July of 2022, proofing the engine for flight.