Performance study of a repetitively pulsed two-stage plasma propulsion engine Final report
Performance Study of a Repetitively Pulsed Two-Stage Plasma Propulsion Engine Final Report
Two Stage Potassium Test Turbine Quarterly Progress Report No. 14, Aug. 8 - Nov. 8, 1964
Aerodynamic Design - Model II Turbine M-1 Fuel Turbopump Assembly
Study of Parametric Performance of a Two-Stage Repetitively Pulsed Plasma Engine (Reppac)
Two Stage Potassium Turbine - 3000 Hour Test Final Report
High Performance Turboalternator and Associated Hardware. 1 - Design of Turboalternator
Continuous measurements of in-bore projectile velocity
Monolithic HEMT LNAS for radar, EW, and COMM
Terrain mapping for a roving planetary explorer
A family of InGaAs/AlGaAs V-band monolithic HEMT LNAs
Optimization of multivariate simulation output models using a group screening method