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"Conditions contributing to stress corrosion [list] photograph."
8 x 10 inch black and white photograph. A photograph of a list of things contributing to stress corrosion. Referenced by "Materials in Space Exploration." Is part of envelope containing photos accompanying C. E. Cataldo paper "Materials in Space Exploration." -
"Conductor's Report of Army, Navy Or Marine Personnel Carried" from the Atlanta and West Point Rail Road Company.
The conductor's report notes 158 passengers in coach from Augusta to Atlanta. -
"Configuration Management-Definition".
Configuration management: Definition, requirements, organization, policy and procedure documents, contractual documents. -
"Contract Status Report."
Saturn funded contracts in excess of $100,000. Lists contracts by contract numbers. Gives contractor, value, place of performance and scope of work.; There is a burned stripe across one page. -
"Contractor Program Procedure".
Outlines various procedures for Saturn V contractors. -
"Contractor Program Procedures".
A collection of various procedures. Archive copy is a photocopy. There is no continuous numbering in this document. -
"Contracts & Pricing: Saturn S-II Program".
Indicates the various levels and responsibilities within the Saturn V pricing and contract personnel. September 3, 1968.; Approved S. L. Weinberg. -
"Contracts for Saturn Upper Stages S-IV and S-V".
Details contracts for upper stages of Saturn IV and Saturn V and includes illustrative appendixes. Archive copy is a photocopy. -
"Cool Names For Women?; The Cold Facts: They're Not"
Uses doll, chick and fox to convey inappropriate terms for addressing women -
"Corrosion Problems Associated with Space Launch Vehicles".
A document reporting various space vehicle corrosion issues. Original is photocopy. -
"Corrosion problems associated with the Saturn space vehicles."
Corrosion problems associated with space vehicles, in general, are discussed as contrasted to those problems experienced with structures in an earth atmosphere. Primary emphasis is placed on structural alloys in this discussion, although some corrosion failures experienced in various mechanical components are described. General corrosion prevention measures are indicated, and solutions to specific corrosion failures described. Major failures experienced have been attributed to stress corrosion cracking, rather than general or galvanic type corrosion. Most such failures have occurred with only five different materials: three aluminum alloys - 7075-T6, 7079-T6, and 2024-T6; and two precipitation hardening stainless steels - 17-7PH and AM 355. Corrective actions were different in each case, but involved either a complete change to another material, a change to a different temper of the same alloy, or a modification of the heat treatment and/or general processing techniques. General conclusions are that the types of failures described could be avoided by: a more suitable selection of alloys in the initial design, a realistic review of the environments that could be encountered in the service lifetime of the component, lowering stresses, improving process controls, and effecting better familiarization of design personnel with the with the overall stress corrosion problem in an effort to reduce human error.; Preprint 18e.; Materials for re-entry and spacecraft systems - spacecraft materials.; Materials Conference, Philadelphia, Pennsylvania, March 31 - April 4, 1968. -
"Cotton Market, Huntsville, Ala."
The photo shows the north side of courthouse square looking east in downtown Huntsville. The Madison County Courthouse can be seen at the right of the photo. -
"Countdown to Liftoff".
This is an article from the Boeing Magazine. The Archive copy is a very poor photocopy and is difficult to read.; About the time the S-IC-1 booster is lifting the first Apollo/Saturn V from the launch pad on its maiden unmanned flight next year, a Boeing systems test crew will begin static testing the S-IC-4 at Devils Swamp, Mississippi (MTF). Starting with S-IC-4, all Saturn V first stage boosters will be captive fired at MTF. At present, S-IC firings are conducted by MSFC's test laboratory at Huntsville. The first flight stage, the S-IC-1, was placed in the static test stand on 24 January 1966 and completed its test program 25 Feb. It was removed from the stand March 14 and is undergoing post-firing checkout. it is due to be shipped this summer to KSC where it will be mated to the two upper stages of Saturn V, the IU and Dummy Apollo payload. The S-IC-2 went into the static stand on March 22 and is being tested during April The S-IC-3 also will be tested at Huntsville in 1966. The job of putting the world's largest and most powerful rocket together will be accomplished in the world's largest building, the 52-story vehicle assembly building. -
"Countdown trials start for launch."
News article detailing how the crew of the Apollo 8 are preparing for launch with a "dry run." -
"Craft destined for use in lunar landing mission."
News article detailing how the Apollo spacecraft 107 command modules are planned to be used in future space-missions. -
"Crew Briefing : Instrument Unit Stage Presentation".
Document outlining different slides of a presentation containing numerous organizational charts, diagrams and bullet-list points. -
"Crew Briefing : Instrument Unit Stage Presentation".
Document outlining different slides of a presentation containing numerous organizational charts, diagrams and bullet-list points. -
"Currency Exchange Control Book."
The book includes details about Salmon's exchange transactions while stationed in Europe in spring 1946. -
"Current Journal Subscriptions 1962 - 1963."
This is a typed list of the journal subscriptions for the library in 1962-1963 with additional journals written at the bottom of the list. At the top of the document, there is a written note to "Dr. Roberts," presumably history professor Frances Roberts, requesting she renew all of the subscriptions. -
"D5-13197 manufacturing plan: AAP."
This Manufacturing plan is prepared in response to the Apollo Applications Program request for proposal No. 1.1.; PURPOSE: The purpose of this document is to present a Boeing plan for the manufacturing effort required to provide hardware and support for the installation and checkout of Experiment Packages and related equipment in the Apollo Systems Modules. -
"Daily Globe"
March 16 1872 -
"Dangerous Liasons...Sun and Stupidity; Enjoy a Safe Summer"
Different branches of the military on their off time getting into danger -
"Data Sheet J-2 Rocket Engine."
A datasheet describing the function of the J-2 rocket engine. -
"Data Sheet: H-1 Rocket Engine."
News from Rocketdyne. -
"Daytona Beach - Apollo 15 - Traffic Jam."
The Dannenbergs travel down to Daytona Beach, Florida, to see the launch of Apollo 15. The first half shows the resort and Ingeborg sitting by the beach. The second half shows the drive to the launch facility in Cape Canaveral, Florida and the traffic they find upon arrival. 1971. -
"Daytona Beach w/ Ullrichs am Strand in Wasser. 1st Oct week '67."
Konrad, Klaus, Ingeborg, and Betty Dannenberg and little George vacation with the Ullrichs (Rita and Hanns) in Daytona Beach, Florida. They are all shown playing on the beach outside of their resort. 1967. -
"Daytona Beach."
Ingeborg, Konrad, Klaus, and Betty Dannenberg and little George relax by the pool at their resort in Daytona Beach, Florida. The video focuses mostly on George playing with a toy boat both in and out of the pool. 1967. -
"De Lan' O' Cotton."
Front: "De Lan' O' Cotton." -
"Dec. 21 - 4:51 a.m. -One of great explorations of all time begins."
News article detailing how Apollo 8 is ready for launch and the anticipation surrounding it. -
"Decision Procedure for Minimizing Costs of Calibrating Liquid Rocket Engines."
Prior to acceptance of a liquid rocket engine for use in Saturn vehicles, the average thrust of two consecutive tests without an intervening calibration must satisfy specification requirements. The contractor may recalibrate after the first and subsequent tests if he so chooses, based upon decision limits, until the above requirement is met. -
"Denial Is Not A River In Egypt; It's the best way to protect yourself from AIDS"
Egyptian message, heiroglyphic -
"Department of Defense Celebrates; March 1997; Women's History Month"
Various pictures of women in the Armed Forces throughout history -
"Departure fr. Germany, Ffm Airport & Arrival in N.Y. Summer 1960."
Trip to Frankfurt, West Germany. Shows multiple shots of Frankfurt airport as well as taking off and aerial views of Germany. Final shots show touchdown in New York and the reception area inside of a New York airport. "Ffm" is an abbreviation of Frankfurt am Main. 1960. -
"Design and Development of a 1,500,000-Pound-Thrust Space Booster Engine."
Describes the F-1 engine design and components. -
"Design and Development of a Zero-G Vapor Liquid Separator For Use in Cryogenic Fluid Power Systems."
During long coast periods of zero-gravity, storage vessels for the cryogenic liquids proposed for use in some power transmission systems undergo random distribution of the liquid and vapor phases therein. Thus, when heat flow into the vessel causes the vessel pressure to build-up requiring venting to maintain a safe value, the likelihood of venting the valuable liquid phase, as well as the vapor, results. To preclude this eventuality, various devices for separating the liquid and vapor phases and venting just the vapor have been studied and carried into the experimentation stages. -
"Design and Use of Fault Simulation for Saturn Computer Design."
Describes different aspect of the Fault Simulation for Saturn computer design. -
"Design Concepts of Ground DDAS in Saturn 1B/V ESE."
In the Saturn IB/V programs the sheer quantity of data required for computer processing and ESE display makes it necessary to provide an efficient data acquisition system. For much of the data originating in the launcher this requirement is satisfied by the Ground Digital Data Acquisition System (DDAS). This paper provides a technical description of the Ground DDAS with emphasis placed on the unique design concepts of this telemetry system. -
"Design of the Saturn S-IV Stage Propellant Utilization System."
Describes the SIV vehicle and its components. Presented at: IRE International Convention. -
"Design, Development, and Fabrication of a Prototype Hydraulic Transformer."
For presentation to the Society of Automotive Engineers, 16 September 1964, Boston, Massachusetts. ABSTRACT: This paper discusses the design, development and fabrication of a prototype hydraulic transformer, Hydro-Aire Model No. 05-055, performed in fulfillment of the requirements of Contract No. NAS 8-5264 for NASA Marshall Space Flight Center. The Hydraulic Transformer described is designed to pump hydraulic oil at a flow of 100 GPM with a pressure rise of 4000 psi, and does this work by utilizing as a power source the flow of RP-1 rocket fuel at a pressure of 1900 psig. The Hydraulic Transformer built to handle this combination of flows and pressures, unprecedented in such devices, has a weight of only 70 pounds for the first development model. The development of this unit is discussed and future development improvements are mentioned.