MOMENTUM CONTROL OF THE OAO SPACECRAFT UTILIZING THE EARTH'S MAGNETIC FIELD
Use of reaction wheels and nonlinear control for a satellite scanning a small celestial area
The role of manned orbiting laboratories in the exploration of the planets.
Fabrication of the Titanium Transition Ring of the Large Space Telescope (LST)
Report to the Space Science Board on the space science and applications programs
Effect of Power Dissipation on the Platform Temperatures of the L.A.S
50 Years of Mirror Technology Investment at NASA: From Hubble to JWST and Beyond
Satellite Services System Analysis Study. Volume 3A: Service Equipment Requirements, Appendix
Attitude Control of a Spacecraft with a Strapdown Inertial Reference System and Onboard Computer
Stability Criteria for the Oao Coarse Pointing Mode, Part 2 Final Report
Princeton Advanced Satellite Study, Volume I Final Summary Report, 8 Mar. 1965 - 15 May 1966
Overcharge Control of Nickel-Cadmium Spacecraft Batteries Using the Auxiliary Electrode Signal
50+ Years of NASA Mirror Technology Development: From Hubble to JWST and Beyond
50+ Years of NASA Mirror Technology Development: From Hubble to JWST and Beyond
Stability Criteria for the Oao Coarse Pointing Mode, Part 1 Final Report
The Design of a Large Angle Three-Axis Attitude Servomechanism for Spacecraft
Large Astronomical Satellite First Estimation of Thermal Distortions in a Stable Platform
Irradiation of Thermal Control Coatings Final Report, Feb. 1967 - Feb. 1968
Control and Stabilisation of Spacecraft. Volume 1 - Introduction and Seminars
Use of Reaction Wheel Tachometer Feedback in the Coarse Attitude Control Loop of the L.A.S
Feasibility Study of the Ultraviolet Spectral Analysis of the Lunar Surface
Near Earth Asteroid Human Mission Possibilities Using Nuclear Thermal Rocket (NTR) Propulsion
Princeton Advanced Satellite Study Final Report, 8 Mar. 1965 - 15 May 1966