Titan II Storable Propellant Handbook PDF Download
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Author:
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ISBN:
Category : Handbooks, manuals, etc
Languages : en
Pages : 164
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Book Description
"Summarized are the physical properties, materials compatibility, handling techniques, flammability and explosivity, and procedures for storing, cleaning, and flushing the Titan II propellants N2O4 as the oxidizer and a nominal 50/50 blend of UDMH and N2H4 as the fuel. The data presented was derived both from a literature survey and from a test program conducted at Bell Aerosystems Company and at the U.S. Bureau of Mines". -- page iii.
Author:
Publisher:
ISBN:
Category : Handbooks, manuals, etc
Languages : en
Pages : 164
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Book Description
"Summarized are the physical properties, materials compatibility, handling techniques, flammability and explosivity, and procedures for storing, cleaning, and flushing the Titan II propellants N2O4 as the oxidizer and a nominal 50/50 blend of UDMH and N2H4 as the fuel. The data presented was derived both from a literature survey and from a test program conducted at Bell Aerosystems Company and at the U.S. Bureau of Mines". -- page iii.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 119
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Book Description
Author: RALPH R. LIBERTO
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
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Book Description
Summarized are the physical properties, materials compatibility, handling techniques, flammability and explosivity, and procedures for storing, cleaning, and flushing of the Titan II propellants. These propellants consisted of N2O4 as the oxidizer and a nominal 50/50 blend of UDMH (unsymmetrical dimethylhydrazine) and N2H4 as the fuel. The data presented were derived both from a literature survey and from a test program conducted at Bell Aerosystems Company and at the U.S. Bureau of Mines. (Author).
Author: Ralph R. Liberto
Publisher:
ISBN:
Category : Matter
Languages : en
Pages : 86
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Book Description
Tests were conducted to determine the effects of the Titan II propellants on metals and non-metals and the effects of metals on fuel decomposition. The Titan II propellants are N2O4 as the oxidizer and a 50/50 blend of UDMH and N2H4 as the fuel. The fire hazards of various materials were determined during drip tests with N2O4 and 50/50 fuel blend separately. Storability data is presented for the fuel blend at 60 + or - 5 F. Also, fuel blend separation data was determined after storage at 60 + or - 5 F. Presented is the data from the U.S. Bureau of Mines regarding flammability characteristics of 50/50 fuel blend - N2O4 - air - water mixtures. (Author).
Author: Aerojet-General Corporation. Liquid Rocket Plant
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages :
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Author: Wyle Laboratories
Publisher:
ISBN:
Category :
Languages : en
Pages : 236
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 720
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Author:
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 86
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Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 136
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Author: United States. Dept. of Commerce. Office of Technical Services
Publisher:
ISBN:
Category :
Languages : en
Pages : 850
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