Transonic flutter investigation of models of a proposed variable-sweep wing
Aerodynamic Analysis of Tektites and Their Parent Bodies
Program 162.Aerospace Ground Equipment. Volume II. Checkout Equipment
IGNITER, SPARK, AERONAUTICAL ENGINE (HIGH TENSION)
Computer Program Design Specification. Flight 1501. Milestone IV. 11 December 1961
Personnel Planning Information for Point Arguello Launch Complex 2
Casualty Analysis, Manning Analysis and Machinery Space Arrangements
Rain Erosion at Subsonic and Supersonic Speeds: An Annotated Bibliography
A SIMPLIFIED STATISTICAL MODEL FOR MISSILE LAUNCHING - III
A Simplified Statistical Model for Missile Launching - II
TECHNIQUES FOR PREDICTING LOCALIZED VIBRATORY ENVIRONMENTS OF ROCKET VEHICLES
Statistical Filtering of Space Navigation Measurements
INFLUENCE OF WEIGHT PARAMETERS ON THE PROPULSION REQUIREMENTS'' OF ORBIT-LAUNCHED VEHICLES
Determination of trajectory parameters relative to various AROD ground stations