"Klaus returns from Navy cruise 1963 Atlanta."
Dannenberg, Konrad
German Americans
Atlanta (Ga.)
Klaus Dannenberg returns from sea and meets Konrad and Ingeborg in Atlanta, Georgia. While there, they stay at a Howard Johnson Inn and tour around Atlanta. 1963.
University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama
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Home movies
Moving Image
"Klaus w/ the Navy, departure fr Hv 13 July '63."
Klaus Dannenberg departs to join the U.S. Navy. Shown are Ingeborg and Konrad seeing him off before he boards a flight. Summer 1963.
Interviews
Audio
"Klaus' Confirmation, Church Da.-Feier at w/Huetz's + Katzenshots."
Cats
Confirmation
Huntsville (Ala.)
Madison County (Ala.)
First half of film shows Klaus Dannenberg being confirmed as well as the confirmation celebration at the Dannenbergs' house. Second half shows the new litter of kittens from the Dannenbergs' cat. Winter, 1957/58.
Graduation ceremonies
Auburn University
Auburn (Ala.)
Lee County (Ala.)
Shows the first part of Klaus Dannenberg's graduation from Auburn University. Film shows the in-laws going into the stadium and sitting down, as well as the graduates proceeding into the stadium. 1967.
Film from Klaus Dannenberg's graduation from Auburn University. Shown are a few clips from the president of the college, Klaus walking up to receive his degree, and Klaus meeting with family and friends afterwards. 1967.
Amusement parks--Equipment and supplies
This advertisement provides images, features, and specifications for the turnstile.
Perey Turnstile Company
Advertisements
Fliers (Printed matter)
Still Image
Text
Saturn project
Cape Kennedy launch complex
Astronautics
Testing
Apollo project
The John F. Kennedy Space Center (KSC) Apollo/Saturn V Development/Operations Plan, K-PM-0, establislies the requirement for an Apollo/Saturn V Master Test Plan (MBP). This document, prepared by the Saturn Systems Office.
John F. Kennedy Space Center
Test Plans
Umbilical towers
illustration of the L-UT/Armb umbilical tower
Illustrations
"Launch Complex 34 Facilities Fact Sheet 05."
Article detailing the different aspects of the Launch Complex 34 facilities.
Articles
"Launch Complex 37 Facilities Fact Sheet."
Project management
"Launch Complex 39 Facilities Fact Sheet 03."
Launch complexes (Astronautics)
Launching
"Launch Control and Checkout Equipment (LCCE) [photograph]."
Automatic test equipment
Ground support equipment
Ground support systems
Space vehicle checkout program
Description of an 8 x 10 inch black and white photograph.
United States. National Aeronautics and Space Administration
Descriptions
"Launch Information: Saturn S-IV and the RL10 Engine."
RL-10 engines
Rockets (Aeronautics)--Launching
Liquid propellant rockets
Saturn S-4 stage
The RL10, which powers the National Aeronautics and Space Administration' s Saturn S-IV, is the newest propulsion system to be put to work in advancing our nation's space effortr On November 27, 1963, a pair of RLlO's successfully powered a five-ton Centaur space vehicle in earth orbit in the first flight demonstration of the outer space powerplant which uses high-nenergy liquid hydrogen as fuel. A six-engine cluster of RLlO' s, generating a total of 90, 000 pounds of thrust, powers the Saturn S-IV stage. The 15, 000 pound-thrust engine was designed and developed for NASA's Mar shall Space Flight Center at Pratt & Whitney Aircraft's Florida Research and Development Center, 20 miles northwest of West Palm Beach.
Pratt & Whitney Aircraft Company. Florida Research and Development Center
Reports
"LAUNCH OF THIRD MANNED SKYLAB MISSION."
Merritt Island (Fla.)
Skylab Program
Skylab 4
Gibson, Edward G.
Carr, Gerald P.
Pogue, William R.
Saturn launch vehicles
University of Alabama in Huntsville Archives and Special Collections, Huntsville, Alabama
Skylab Document Scanning Project Metadata
One-Sheet Posters
"Launch Vehicle Engines Project Development Plan."
F-1 rocket engine
H-1 engine
J-2 engine
Liquid propellant rockets--Design and construction
Liquid propellant rockets--Testing
Ullage rocket engines
This revised edition of the Launch Vehicle Engines Project Development Plan supersedes the issue dated July 1, 1965. Significant changes which have been made are:- Removal of classified data to permit publication as an unclassified document; - Removal of material applicable to the RL-10 Engine Project which was transferred to the Lewis Research Center effective May 1, 1966; - Elimination of detailed schedules which quickly become obsolete; - Punched for maintenance in loose-leaf 3-ring binders and for ease in updating material through issuance of replacement sheets. Binders are not furnished. The information in this document is current to January 1, 1967.; The Launch Vehicle Engines Project Development Plan is established in accordance with requirements of NASA General Management Instruction 4-1-1, Planning and Implementation of NASA Projects, and OMSF Instruction MP 9320.044, Preparation and Revision of Program/Project Development Plans (PDP's). The Plan, herein referred to as the PDP, has been developed within the scope of current Apollo Projects Approval Documents (PADS) and will be maintained by the Engine Program Manager to identify program requirements, responsibilities, tasks, and resources, and time phasing of major actions required to accomplish the Engine Program.
George C. Marshall Space Flight Center
United States. National Aeronautics and Space Administration.
The primary mission objective of the 5-2 Engine Project is to continue development of a liquid oxygen/liquid hydrogen engine. capable of high-altitude restart. Both Saturn IB and Saturn V vehicles will use the J-2 engine; the S-IVB stage of Saturn IB vehicles and S-IVB stage of Saturn V vehicles will be equipped with a single J-2 engine. The S-I1 stage of Saturn V vehicles will use a cluster of five J-2 engines. Figure 1-3 illustrates these stages.
Design Analyses
"Launch Vehicle Recovery System Requirements."
Recovery
The primary considerations in the design and development of a recovery system applicable to present expendable first stage launch vehicles are discussed. The general requirements that define the essential characteristics of a feasible recovery system are derived from three critical phases during flight. The degree of criticalness is primarily influenced by the conditions at stage cutoff and separation. The three critical phses of flight are broken down into the following: (1) conditions and requirements between stage separation to re-entry; (2) re-entry; and (3) terminal descent and landing.
Barraza, R. M.
launvehirecosystrequ_061407154402.pdf TWO COPIES
"Lethal Weapons Too; Classifed Information, Even on a Fragile Disk, Is Deadly in Wrong Hands.; Safeguard it!"
Department of Defense poster
United States--Department of Defense
Classified documents
Firearms
Floppy disks
Department of Defense
The University of Alabama in Huntsville M. Louis Salmon Library
Posters