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"Contractor Program Procedure".
Outlines various procedures for Saturn V contractors. -
Contractor Program Procedures: Contract NAS8-5608; DRL 067, Line Item 7; DRL 007, Line Item 7.
The document is a Boeing manual. It contains operating procedures and directives specifically for the Launch Sytems Branch. -
Tiere der Urwelt: in 30 Kunstblättern nach wissenschaftliche Material bearbeitet.
This set of illustrated cards includes thirty color prints of various animals of the prehistoric world. The Theodor Reichardt Cocoa Company produced five different series of these cards in the early twentieth century. While the cover indicates that this volume contains cards from series 1a, it also includes cards from series 1 and series 2a. Many of the pages show notes made in ink by science writer Willy Ley, the book's original owner. -
"Assessment of Risk for Engineering Change Decisions."
This document includes the current basis for approval of ECPs, fatigue life after stress reduction, and other probability and comparative risk assessments. On the first page there is an inscription, "By E.L. Bombara NASA-MSFC." -
List of supervisors for train travel groups.
The list provides the symbols of unit designation and the supervisors for particular groups and their destinations. -
"Redstone Arsenal 1972 Unofficial Guide."
This guide to Redstone Arsenal contains a history of the Arsenal, complete with pictures of "Army Missiles of the Past" and details about the Army Commands stationed there, as well as descriptions of the amenities, facilities, and social opportunities available on base and in the Huntsville area. -
Photo of the lunar drill team.
The back provides a description for the photo reading: "Luncar Drill team consultants, all seated, in Research Projects Lab." -
"Development of LOX/RP-1 Engines for Saturn/Apollo Launch Vehicles."
The development of liquid rocket engines follow similar patterns regardless of engine size. During the development of the H-1 and F-1 engines, many problems were encountered. Methods of solving the combustion instability problem are discussed. A description is given of the major components of each engine, outlining their unique features. The requirements for an insulation cocoon are discussed. Problems associated with materials substitution are provided; also highlighted is the fact that problems occur after engine deliveries and require continued development support. Safety features incorporated on the engines are mentioned. Solution to problems encountered in flight are discussed. Upratings of both engines systems are presented graphically.; On the NASA Technical Reports Server (NTRS) unclassified. Can also be found on AIAA. -
Development of LOX/RP-1 engines for Saturn/Apollo launch vehicles.
The development of liquid rocket engines follow similar patterns regardless of engine size. During the development of the H-1 and F-1 engines, may problems were encountered. Mehtods of solving the combustion instability problem are discussed.; AIAA 4th Propulsion Joint Specialist Conference, Cleveland, Ohio, June 10-14, 1968.; Also available on NASA Technical Reports Server (NTRS) as unclassified. Can be ordered. Also on AIAA. -
"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.