Fault-Tolerant Reduced-Attitude Control for Spacecraft Constrained Boresight Reorientation
High-Gain Spacecraft Antenna Design and Development Final Report
Manned Spacecraft Systems Cost Model, Volume III. Technical Report, Apr. 1965 - Jun. 1966
Energy-method estimates of response to inflight dynamic loads.
Response-to-noise studies of some aircraft and spacecraft structures.
Mariner Mars 1964 basic structure, design and development
Surveyor Spacecraft a-21 a Model Description
A combined system concept for control of the meteoroid hazard to space vehicles.
Flexural rigidity of spacecraft laminates.
Devices for controlling thermal gradients in spacecraft structures
Mariner MARS 1964 Mechanical Configuration
Real-Time Nonlinear Attitude Control System for Nanosatellite Applications