X-33 Hypersonic Aerodynamic Characteristics
WOBBLE: A Proposed Mission to Characterize Past and Present Water on Mars
Wear Mechanisms in Electron Sources for Ion Propulsion, 2: Discharge Hollow Cathode
Wall interference effects in wind tunnel testing of STOL aircraft.
Voltage breakdown in spacecraft flight systems - A design problem
Use of electroexplosive devices in the Active Seismic Experiment.
Two Reconfigurable Flight-Control Design Methods: Robust Servomechanism and Control Allocation
Transonic Shock-Wave/Boundary-Layer Interactions on an Oscillating Airfoil
Trajectory analysis of a Grand Tour mission to the outer planets.
Time required for an adequate thermal-vacuum test of flight model spacecraft.
Thrust transient prediction and control of solid rocket engines.
The X-43A Flight Research Program: Lessons Learned on the Road to Mach 10
The unpowered rotor - A lifting decelerator for spacecraft recovery.
The technology of ground stations in the deep space network from 1958 to 1968.
The SDP-3 - A computer for use on board small scientific spacecraft.
The role of space simulation testing in the development of Mariner spacecraft
The role of man in an Observatory and Laboratory Spacecraft
Thermionic reactor systems for electric propulsion
Thermionic reactor electric propulsion spacecraft for unmanned outer planet exploration
Thermal-vacuum tests of all-up spacecraft for the Apollo Program
Thermal Performance of an Annealed Pyrolytic Graphite Solar Collector
Thermal design evolution and performance of the Surveyor spacecraft.
Theoretical and practical implications of the bidirectional reflectance of spacecraft surfaces.
The objectives for manned planetary missions.
The NASA-ERC V/STOL avionics systems technology program.
The MSFC experimental development program for lunar surface navigation equipment
The modularization approach to living and working in near earth space
The mission of Mariner Mars '69.
The Integrated Airport Competition Model, 1998
The impact of the flight specifications on semiconductor failure rates.
The History of Solid-Propellant Rocketry: What We Do and Do Not Know
The effects of crew motion on the attitude of a manned orbiting-spacecraft.
The CARD Study - What is its impact
The aerodynamics of high lift illustrated by augmentor-wing research
The Advanced Reusable Technologies Project
Testing and analysis of the lunar module supercritical helium pressurization system.
Test facility for simulation of system- environment interaction during Martian entry.
Temperature compensation versus temperature control of inertial instruments
Technological factors in short haul air transportation
System studies of fusion powered pulsed propulsion systems
System design of an outer planet spacecraft for long-life reliability
Switched-mode adaptive terminal control for propulsive landing of nonlifting spacecraft