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Silent, 3.75 KW Liquid Hydrocarbon-Air Fuel Cell Powerplant. Volume II. Figures and Tables
Study of Arc-Jet Propulsion Devices Final Report, 20 Nov. 1964 - 19 Dec. 1965
20-Hour Follow-on Flight Test Program, XV-9A Hot Cycle Research Aircraft
Air Heating by a Rotating Arc with Cold Gas Flow Transverse to the Axis of the Arc
Communist Chinese Rocket Propulsion Technology: Compilation of Abstracts
Introduction to Ballistics Rockets and Rocket Ballistics (Selected Parts)
Notes on the Selection of Refrigerants for Aircraft Vapour Cycle Cooling Systems
Performance Evaluation of a Liquid-Shrouded Cryogenic Storage System
Study of Thermoelectric Cooling of Electronic Equipment Final Report
The a.R.L. Supersonic Propulsion Test Facility - Thermodynamic Design of Regenerative Heat Exchanger
The London Postal Region Dimmed Headlight Experiment
High Speed Impact Test on a 40FT. Lighting Column Fitted with a Break-Away Joint
Space Applications of Cryogenic Technology
Aircraft Instrument and Cockpit Lighting by Red or White Light
A Solar Cell and Heater System to Reduce the Temperature Variation of Units in a Spacecraft
Investigation on the Cooling of Exhaust Gas by Direct Contact Between Exhaust Gas and Water
Thermal Insulation of Small Instrumentation Probes
An Analytical Solution of the Impact Behavior of Luminaire Support Assemblies
Investigations in Chemical Rocket Propulsion Final Report, 1 Jul. 1964 - 31 Dec. 1967
Advanced Rocket Engine--Storable. Phase 1 Interim Final Report. Part 2. Sections 5 Through 8
Transpiration Cooling System Development for Reentry Vehicles
Vuilleumier Cycle Cryogenic Refrigerator Development
Air Cooler for Hypersonic Wind Tunnels
System Validation Test. Lem Crew Compartment Cooling Unit, Launch Complex 37, Launch Area B
Evaporative Cooling Garment System (Ecgs), Part 1 Final Report
300-Ekw Thermionic Reactor Design Study. Final Report
Analysis of Three-Fluid, Crossflow Heat Exchangers
Exploring in Aerospace Rocketry. 7 - Liquid Propellant Rocket Systems
Development of a Chemical Heater for a MARS Rough-Landing Capsule
Computer Program for APOLLO Fuel Cell Radiator-Condenser Cooling System Analysis
Acceptance Testing of the Cold Air Supply to Third Stage and Satellite, Launcher 6 A, Woomera
DC Regulator for Low Pressure Mercury Lamps (Pen-Ray)