Effect of Engine Skew on Directional and Lateral Control Characteristics of Single-Engine Airplanes
Theory of Helicopter Damping in Pitch or Roll and a Comparison With Flight Measurements
Application of a Liquid Propellant Rocket as a Turbojet Thrust Augmentation System
Basic Captive Test Plan Sycamore Stand S-2
Accident Investigation Report Missile 5A Static Test Stand 1-1
An Investigation of the Jetevator as a Means of Thrust Vector Control
Captive Testing of Missile 14A at Mstsan-1, Edwards Air Force Base, Edwards, California
Small Rocket Lift Device. Phase I. Design, Fabrication, and Static Testing
Flight Test Working Group, Flight Test Report Atlas Missile 60D 2 Jul 1960, Ws107a-1
WS 107A-1Flight Test Working Group Flight Test Report, ATLAS Missile 4E, 20 November 1960
Analog Simulation of a Pilot-Controlled Rendezvous
Low-Thrust Vehicle Guidance Study: Volume II, Parts II and III