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Laboratory Investigation of Countermeasures Receiving Set AN/ALR-2 (Xn-2)
Xsm-65D Missile Impact Predictor System Checkout Description and Plan
Evaluation Test of High Pressure Relief Valves 3200 and 6500 Psig
Point Return from a Lunar Mission for a Vehicle that Maneuvers Within the Earth's Atmosphere
X-Ray Image System for Nondestructive Testing of Solid Propellant Missile Case Walls and Weldments
X-Ray Image System for Nondestructive Testing of Solid Propellant Missile Case Walls and Weldments
X-Ray Image System for Nondestructive Testing of Solid Propellant Missile Case Walls and Weldments
Cellular Growth and Tissue Radiosensitivity: Cell Studies in Vitro and General Concepts
Peripheral mechanisms of human temperature sensitivity final report, 1 sep. 1961 - 31 aug. 1964
Differential Spectral Sensitivity in the Optic Tectum and Eye of the Turtle
An Amplifier for Use with Solid State Radiation Detectors in Spacecraft Applications
Spark Counter for Recording Particles of Cosoc F Cosmic Radiation
Sensitivity of explosives and propellants to impact and friction
A visual flight investigation of hovering and low-speed vtol control requirements
Effect of Liquid Nitrogen Dilution on LOX Impact Sensitivity
APOLLO Logistics Support Systems Molab Studies. TV Subsystem Studies for a Lunar Mobile Laboratory
A Visual Flight Investigation of Hovering and Low-Speed VTOL Control Requirements
Unmanned Systems to Evaluate the Martian Environment Condensed Summary Report
Our Investment in Space to Bring Manifold Returns First Supplement
Study of Unmanned Systems to Evaluate the Martian Environment. Volume I - Sensitivity Analysis
Lunar Navigation Study, Sections 8 Through 10 and Appendices Final Report, Jun. 1964 - May 1965
The Dynamic Environment of Spacecraft Surface Transportation
The Dynamic Environment of Spacecraft Surface Transportation
The dynamic environment of spacecraft surface transportation
Solid Propellant Rocket Motor Performance Computer Programs Using the Group Transformation Method
The Development of Sterilizable Image Dissector Tubes Final Report, 15 Apr. 1964 - 15 May 1966
Stellar Acquisition Feasibility Flights (Staff), Volume II - Technical