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Particle Trajectory Program for Re-Entry Vehicle Flight Test Data Processing
Post Flight Digital Simulation of the Atlas 40-D Missile
Experimental Evaluation of Cooperative Collision Avoidance System
Range Safety Trajectory and Dispersion Information for the SM-65-7F Flight Test Vehicle
The Optimization of Multi-Stage Orbit Transfer Processes by Dynamic Programming
Range Safety Trajectory and Dispersion Information for the SM-65-40E Flight Test Vehicle
Merchant Ship Automation Study. Appendices to Automatic Ship Control and Communications Systems
Computer Program Subroutines. Flight 1202. Milestone xi
Computer Program Design Specification. Flight 1501. Milestone IV. 11 December 1961
A Simulator Investigation of a Self-Adaptive Pitch Damper for a High Performance Fighter Aircraft
Computer Program Design Specifications. Flight 2202 Milestone IV, 23 March 1962
A Theoretical Performance Investigation of an Afterburning Turbofan Engine. Appendix
Statistische Probleme in der Flugmechanik (Statistical Problems of Flight Mechanics)
OPTIMUM INTERPLANETARY RENDEZVOUS WITH POWER-LIMITED VEHICLES
Simulation of Helicopter and V/STOL Aircraft., Volume I: Helicopter Analysis Report
Studies Performed to Determine Suspension Needs for Lance Limited Mobility Launcher
On Direct Sums and Tensor Products of Non-Linear Programs
Dynamic Programming Analysis of Multiple Guidance Corrections of a Trajectory (Revision No. 1)
Optical ascent into orbit - a new look at an old problem.
A Dynamic Programming Approach to Bid Evaluation in Procurement
A Preliminary Investigation of the Use of Inertial Guidance for CO-Planar Orbital Rendezvous
Orbital Transfer by Optimum Thrust Direction and Duration
Flight Analysis of Approach and Landing Guidance Elements of Heliport Lighting Patterns
The Effect of Forward Speed on Damping for a Variety of Ship Types as Calculated by Thin Ship Theory
Control Systems Theory Applied to the Re-Entry of Aerospace Vehicles-II
Simulation of Helicopter and V/STOL Aircraft. Volume V. Summary of Final Results
A plan for validation and verification of Apollo flight computer software