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"Furnace Brazing the F-1 Thrust Chamber for Apollo."

This work described in this report was performed for the National Aeronautics and Space Administration under contract NASw-16. Rocketdyne is now building the F-1 engine for the Apollo lunar mission. Five F-1 engines, each capable of developing 1-1/2 million pounds of thrust will power the first stage of the launch vehicle of Saturn V.

"The significance of parameters affecting the heat transfer to the liquid hydrogen in the Saturn S-IVB stage for the lunar orbit rendezvous mission."

The Saturn S-IVB stage has a requirement for orbiting around the earth for up to 4.5 hours with approximately 60 percent of its initial propellant remaining at the end of the coast (prior to restart) . Extensive analyses must be performed to insure that this requirement is met. Both the maximum and minimum heat transfer rates are important because the maximum rates affect the hydrogen boiloff losses and thus the initial propellant loading requirements. The minimum rates are important because the boil off gases are used to maintain a minimum axial thrust level by venting the gases continuously through aft facing nozzles. This provides for a settling of the propellant throughout the orbital coast and alleviates the need for periodically venting the tank under zero gravity.

"Development of the Saturn S-IV and S-IVB Liquid Hydrogen Tank Internal Insulation."

In April of 1960 the Douglas Aircraft Company was awarded a contract to develop the second and uppermost stage for the Saturn I space booster. In order to realize the high specific impulse available, this stage, called the S-IV, was to utilize liquid hydrogen and liquid oxygen as the propellants. After burn-out of the first stage, the S-IV Stage was to ignite its engines at an altitude of approximately 200,000 feet, burn for approximately 8 minutes, and inject a 20,000 lb spacecraft into a low earth orbit. This program represented Douglas's first major endeavor with liquid hydrogen. It was necessary to develop an insulation for the S-IV Stage that was capable of withstanding the thermal shock associated with loading, could provide adequate insulative properties to limit the flow of heat into the hydrogen, and was of minimum weight. This latter fact cannot be over emphasized because every extra pound of insulation is one less pound of available payload weight.

AIDS in Alabama in 1994, Decatur Daily

A chart of the AIDS statistics in Alabama from a 1994 edition of the Decatur Daily. The numbers were sourced from HIV-AIDS Division, Alabama Department of Public Health.

Saturn Launch Vehicles Astrionics System Handbook, 2nd revised edition.

This updated edition of the Astrionics System Handbook instructs, "The enclosed pages change, delete, or supplement the information in the Astrionics System Handbook (1 August 1965). Insert these pages and destroy the pages they replace."

Saturn Launch Vehicles Astrionics System Handbook.

Includes change pages. Contract NAS8-14000. Second revised edition. V66-15610. NASA-CR71607. The introduction notes, "This second revised edition of the Astrionics System Handbook has been developed under the direction and overall supervision of Dr. Rudolf Decher of the Astrionics Systems Engineering Office. This description of the Saturn Astrionics System has been generated by personnel of the Astrionics Laboratory, the staff of the Astrionics Systems Engineering Office, and by personnel of the International Business Machines Corporation working under Contract NAS8- 14000. The handbook will be updated and expanded as it becomes necessary due to changes or refinements in the system concept and hardware. Sections not contained in the first release of this document will be made available within three months." Signed by Ludie G. Richard, Chief, Systems Engineering Office, Astrionics Laboratory. The document is missing pages in the following locations: Chapters 8, 9, 12. Sections 15.2, 15.3, 15.4-1 thru 15.4-16, 15.5-1 thru 15.5-2, 15.5-5 thru 15.5-8.

"Project Dynasoar (u): a report bibliography."

Projected by D.L. Christiansen, DLC- 5/2/69-Memo.; Search control No. 015416.; For Scientific and Technical Information, Cameron Station, Alexandria, Virginia.; Unclassified.; Pages in this bibliography are not numbered.

"Project Thor (u): a report Bibliography."

Unclassified control No. 015415.; Requested by D.L. Christensen, DLC-5/2/69-Memo for Scientific and Technical Information, Cameron Station, Alexandria.

"Pershing (u): a report bibliography."

List of unclassified reports.

Space Stations/Platforms/Workshop (U): A Report Bibliography.

The document is an annotated bibliography of reports from Requested by D. L. Christiensen. 2

"Saturn : DMS market intelligence report."

Lists numerous costs.

"Marshall analysis : DMS Market Intelligence Report."

Lists numerous costs.

"Saturn V First Stage Annual Progress Report: Fiscal Year 1968."

The report covers June 30, 1967 through June 27, 1968: Contract NAS8-5608, Schedules 1 and 1A, July 27, 1968. Prepared by J. P. Delaloye, Management Reporting and Analysis; Supervised by D. G. Valentine, Management Reporting and Analysis; Approved by R. F. Terry, Program Reports; D. H. Creim, Michoud, Program Planning and Reporting Manager; E. K. Cooper, S-IC Program Executive.