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A Brief Overview of the Effects of Impact Damage to Rocket Motor Cases
A critical discussion on the planning considerations of electric propulsion for space missions
Advanced digital circuit R and D evaluation Final report, 3 Oct. 1964 - 30 Sep. 1965
Advanced Planetary Probe Study Mid-term technical progress report
Advanced post-saturn earth launch vehicle study executive summary report
Advanced systems checkout design First quarterly progress report, Jun. 29 - Sep. 29, 1965
Advanced systems checkout design Fourth quarterly progress report, Mar. 30 - Jun. 29, 1966
Aeroelastic load growth effects on Saturn configurations
A feasibility study of head-end steering for a simplified manned space vehicle
Analysis and Design of Space Vehicle Flight Control Systems. Volume I - Short Period Dynamics
Analytical study of launch vehicle component level simulation, 26 March - 26 November 1965
An analysis of chemical upper stages for nasa scientific missions
A performance study for the application of the Saturn V to high energy earth escape missions
Application of Airbreathing Propulsion to Reusable Launch Vehicles
Approach in Achieving High Reliability of the Saturn Class Vehicles
Armstrong Research, Technology, and Engineering Accomplishments 2014
AS-202 launch vehicle operational flight trajectory
A study of launch-vehicle responses to detailed characteristics of the wind profile
Atlas/Centaur flight performance reserve Monte Carlo analysis AC-7
Atlas/Centaur launch-on-time study Final report /Surveyor mission/
A variational method for multistage launch vehicle optimization
Bending mode acceleration influence on pilot control of flexible booster dynamics
Booster attitude stabilization network synthesis Summary report
Common Bulkhead Joint Development and Evaluation Final Report
Conceptual Launch Vehicle and Spacecraft Design for Risk Assessment
CubeSat Technology Past and Present: Current State-Of-The-Art Survey
Data link equipment for Saturn ground computer systems Final technical summary report
Description and operation of spacecraft in sert i ion thrustor flight test
Design and development of the Castor IIA ROCKET motor Final report
DESIGN CRITERIA FOR ZERO-LEAKAGE CONNECTORS FOR LAUNCH VEHICLES, VOLUME 6 - ENVIRONMENTAL EFFECTS