Study of Ballistic and Metallurgical Characterisitics of Steel Aircraft Armor
The Economics of Preventive Maintenance of Missile Ground Support Equipment
Error Analysis and Performance Optimization of Rocket Vehicle Guidance Systems
Application of a Fast Reactor Concept to Rocket Propulsion, June 15, 1960
STUDIES IN THE FIELDS OF SPACE FLIGHT AND GUIDANCE THEORY. INTRODUCTION
Optimum Interplanetary Rendezvous Trajectories With Power-Limited Vehicles
THREE-DIMENSIONAL LOW-THRUST INTERPLANETARY TRAJECTORY OPTIMIZATION
Optimal multistage rocket flight and other discontinuous variational problems
Retention of human system capabilities during manned space flight
Linear Acceleration Guidance for Lunar Landing and Launch Trajectories
Performance Study of a Repetitively Pulsed Two-Stage Plasma Propulsion Engine Final Report
Studies to Determine Optimum Lunette Load for the Lance Lightweight Launcher
A Trajectory Optimization Technique Based Upon the Theory of the Second Variation
Optimum Shape of a Body of Revolution with Base Drag at Supersonic Speed
Manufacturing Engineering Laboratory's Weld Environmental Control
Eldo Future Program Study 4.1. Eldo C Satellite Launcher Vehicles
Astrodynamics-optimization theory and guidance theory Research achievements review series no. 15-16
Rocket trajectory optimization final technical summary report, mar. 1961 - dec. 1964
Launch vehicle optimization, phase II. VOLUME I - Concept development and application Final report
Special orbits for the exploration of Mars and Venus