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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
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
Effect of Liquid Nitrogen Dilution on LOX Impact Sensitivity
APOLLO Logistics Support Systems Molab Studies. TV Subsystem Studies for a Lunar Mobile Laboratory
Unmanned Systems to Evaluate the Martian Environment Condensed Summary Report
A Visual Flight Investigation of Hovering and Low-Speed VTOL Control Requirements
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
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
A Sensitive S-Band Noise Receiver Developed for the Mariner MARS 1964 Spacecraft Program
Transportation and Handling Shock and Vibration Environmental Criteria
Synthesis of Flight Control Systems Subject to Vehicle Parameter Variations
Compatibility of Polymeric Films with Liquid Oxygen
The Insensitivity of Turbulent Flow to Changes in Reynolds Number and Mach Number
Analysis and Design of Space Vehicle Flight Control Systems. Volume F - Sensitivity Theory
Performance of Two Subliming Solid Propellant Thrustor Systems for Attitude Control of Spacecraft