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Conceptual Launch Vehicle and Spacecraft Design for Risk Assessment
On Applying Finite Elements to Panel Flutter
Improvements on the analysis of shells of revolution by the matrix displacement method.
A matrix-Holzer analysis for bending vibrations of clustered launch vehicles.
Mechanical Impact System Design for Advanced Spacecraft (Misdas)
A Method for Preliminary Estimation of Fatigue Strength in Aircraft Primary Structures
AERO-Astrodynamics Research and Development Research Review No. 1, January 1 - June 30, 1964
Aero-Astrodynamics Research and Development Research Review No. 1, January 1 - June 30, 1964
SPACE FLIGHT HANDBOOKS. VOLUME I- ORBITAL FLIGHT HANDBOOK, PART 2 - MISSION SEQUENCING PROBLEMS
Space Flight Handbooks. Volume 1- Orbital Flight Handbook, Part 3 - Requirements
Space Flight Handbooks. Volume I- Orbital Flight Handbook, Part 1 - Basic Techniques and Data