A Trajectory Optimization Technique Based Upon the Theory of the Second Variation
Optimization of Saturn IB and V mounting and thermal conditioning panels Final report
Optimum Two-Pulse Passage Between Orbits with Small Inclinations and Eccentricities
Astrodynamics-Optimization Theory and Guidance Theory Research Achievements Review Series No. 15-16
Approach in Achieving High Reliability of the Saturn Class Vehicles
Research on the Design of Adaptive Control Systems, Volume 1 Final Report
Trajectory Optimization by Explicit Numerical Methods
Gravity Assist Optimization Technique Applicable to a Variety of Space Missions
Silent, 3.75 KW Liquid Hydrocarbon-Air Fuel Cell Powerplant. Volume II. Figures and Tables
Supersonic transport trajectory optimization example solutions Final report
On the problem of comet orbit determination for spacecraft intercept missions
A Momentum Rule for Optimum Aircraft Performance in the V/STOL Transition Regime