Astrodynamics-optimization theory and guidance theory Research achievements review series no. 15-16
The Cost/Weight Merit Function for Aerospace Hardware Design
Rocket trajectory optimization final technical summary report, mar. 1961 - dec. 1964
Design of optimized three-dimensional thrust nozzle contours
Launch vehicle optimization, phase II. VOLUME I - Concept development and application Final report
Special orbits for the exploration of Mars and Venus
Research achievements in optimization techniques
Mission logic development and trajectory prediction, determination and optimization Final report