PROCEDURE FOR OPTIMIZING GROUND SUPPORT EQUIPMENT AS APPLIED TO FALCON MISSILES
some thoughts on optimum combinations of Wings and Vertical Thrust Generators in VTOL Aircraft
OPTIMIZATION OF PHASE ANGLE AND VOLUME RATIO FOR STIRLING ENGINES
Optimum Joint Design - for High-Temperature Design Honeycomb Panels
Material and Structural Damping for Vibration Control
Design and Test of a Fan Diffuser Bend System Suitable for a Ground Effect Machine
Optimization of Hydraulic Accumulators for Low Temperature Applications
Feed System Problems Associated with Cryogenic Propellant Engines
Charge Stratification by Fuel Injection into Swirling Air
A Computer Analysis of Large Booster Structures for Design Optimization
Evaluation of Dynamic Response Characteristics of a Supersonic Transport Landing Gear System
Increased Reliability Through Spare Parts Optimization
The Cost/Weight Merit Function for Aerospace Hardware Design
Optimum guidance for a low thrust interplanetary vehicle.
Event Monitoring With a Time-Shared Computer Controlled Checkout System
Optimizing the Radar Detection of Clear Air Turbulence
A New Design Concept in Cylindrical Roller Bearings
An Approach to Load Sensing Brake Proportioning for Passenger Cars and Light Trucks
A direct and analytical solution for space flight guidance functions.
The flight path control software system of the Lunar Orbiter.
Optimization problems caused by interaction of guidance and propellant systems.
Optimization problems caused by interaction of guidance and propellant systems.
A general method for determining optimum thrust nozzle contours for gas-particle flows.
Optimal Control System Performance for an A-C Electric Vehicular Drive
Optimal and suboptimal guidance and control for low thrust orbital transfer.
Preliminary Studies of a Supersonic Business Jet
Maintainability Design Review of the AN/SQS-26CX Sonar System
A statistical optimization of the two-impulse transfer maneuver for a fixed-time rendezvous.
Improving Design Quality with Computers - Harvesting Equipment
Rapid determination of near-optimum linear pitch programs for rocket boosters.
Why Has the Medium-Speed Diesel Become Competitive in Marine Propulsion?
A manual optimal guidance scheme using a predictive model.
Optimization of data return from planetary missions by trajectory design.
Optimal payload trajectory characteristics for winged booster vehicles.
Automatic design of optimum Atlas-Agena vehicle trajectories.
Research relating to long-range supersonic cruising aircraft.