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"Management matrix integrating logistics support planning events."
This was found folded inside Configuration Management. Taken from Defense Industry Bulletin, June 1968. Includes an organizational chart and an accompanying bibliography. -
"Management system"
The title has been cut off of document. This was placed inside the document Configuration Management. An organizational chart of plans and critical events related to those plans. -
"Michoud assembly facility and Mississippi test facility : volume II. 4th edition."
This document is the fourth edition of the management charts and photographs maintained in the Management Information Office of the Executive Staff on Michoud Assembly Facility and Mississippi Test Facility. Information on other MSFC activities and facilities will be published in separate volumes. -
"Michoud Assembly facility telephone directory : Boeing Launch Systems Branch, Chrysler Space Division, LTV Range System Div., Mason-Rust Engineering Company."
Telephone directory displaying available channels and how to access them. -
"Michoud operations : historical operations: July 1, 1963 - December 31, 1963."
Historical report from July 1st to December 31st. -
"Milestones in cryogenic liquid propellant rocket engines."
This paper reviews the milestones achieved with cryogenic liquid propellant rocket engines, discusses current technology improvement programs, and projects future engine designs. During the last two decades, these cryogenic rocket engines have played a major role in rocketry and achieved numerous important milestones. These engines power the Vanguard, Redstone, Thor, Atlas, and Titan I vehicles , the Saturn I and Uprated Saturn I vehicles, and will soon be employed in the Saturn V for the Apollo missions. The requirements dictated by these vehicles have necessitated growth from the 27,000-pound-thrust Vanguard engine to the 7,600,000-pound-thrust booster cluster for the Saturn V. Gains in specific impulse have also been significant. The successful application of liquid hydrogen in the Centaur and Saturn upper-stage rocket engines was a major achievement. -
"Minimax control of large launch boosters."
Keith D. Graham is principal mathematician, Systems and Research Center, Honeywell, Inc., 2345 Walnut Street, St. Paul, Minnesota.; Work done under NASA contract NAS 8-11206 from the George C. Marshall Space Flight Center.; ABSTRACT: A method of specifying the gains of a linear controller for a large launch booster using a new application of optimal control theory is described in this paper. Results for a specific example are included. An important control requirement is to maintain cost variables (such as bending moment, engine gimbal deflection, and lateral deviation from desired trajectory) within specified limits in the presence of load disturbances. This requirement is met by using a performance index which depends explicitly on maximum achievable values of the cost variables in a finite time interval. -
"Mission and facilities of Instrument Development Branch."
Describes the purpose and goes of the George C. Marshall Space Flight Center. Instrumental development branch. -
"The Missile gap : a study of the formulation of military and public policy."
A thesis presented to the faculty of the Fletcher School of Law and Diplomacy. In partial fulfillment of the requirements for the Degree of Doctor of Philosophy.; This document is only the abstract of the thesis.; Document includes biographical note and table of contents.; aArchive copy is a photocopy. -
"Mississippi test - torrents of flame."
Description of a photograph of a rocket static test firing.