Preignition Products from Storable Propellants at Simulated High-Altitude Conditions
Investigation of Thermal-Resistant Propellant for Emergency Egress Rockets
Ion Engine Thrust Vector Study Quarterly Report
Concorde - Summary of Thermal Fatigue Tests on Spars Representing Wing Spars or Ribs
The Use of a 35 G Hz Radiometer for Microwave Groundmapping
Computer Program for APOLLO Fuel Cell Radiator-Condenser Cooling System Analysis