TY  - RPRT
TI  - Analysis of Integrated Spacecraft Performance Using A Rotating Detonation Rocket Engine
AU  - M.J. Cooper
AU  - D.E. Paxson
AU  - H.D. Perkins
AU  - J.E. Fittje
UR  - https://ntrs.nasa.gov/citations/20240003814
ID  - 20240003814
ER  -