Problems Encountered During Installation and Operation of a Storable Propellant Facility for Testing of Titan II Components and Systems PDF Download
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Author: Wyle Laboratories
Publisher:
ISBN:
Category :
Languages : en
Pages : 132
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Book Description
Author: Wyle Laboratories
Publisher:
ISBN:
Category :
Languages : en
Pages : 132
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 78
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Book Description
The design and operation of a storable propellants test facility utilizing N2O4 and the Titan II UDMH-N2H4 fuel blend as the fluid media are discussed. Two 6,000-gal stainless steel tanks provided fuel blend storage and similar tanks to store the N2O4. The blending system consisted of a 6,000-gal tank, two 260-gpm pumps for recirculation, and a high turbulence blender. The toxicity of the storable propellants necessitated the inclusion of aspirators, N purge connections, liquid drain valves and isolation valves to facilitate removal of components from the test sections. Similar precautions were provided for component removal from the fuel and oxidizer systems. Waste propellant liquid and vapor neutralization, material compatibility, contamination, leakage, lubricants, seals, and materials are discussed.
Author:
Publisher:
ISBN:
Category : Handbooks, manuals, etc
Languages : en
Pages : 164
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"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 : Science
Languages : en
Pages : 1216
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 684
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Author: Wyle Laboratories
Publisher:
ISBN:
Category :
Languages : en
Pages : 236
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Author: JAMES P. COOPER
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
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Book Description
A stainless steel vapor scrubber was added to the test facility for scrubbing N2H4 vapors. Other minor modifications consisted of the ad ition of gaseous N purge lines, reloca ion of filters, and minor plumbing changes for adapting specific test specimens to the test systems. Evaluation su maries, data, and test procedures are presented in detail for the pre-qualification of Titan II propellant transfer system components. These components include (1) heat exchangers, (2) canned pumps, (3) piston-operated angle globe valves, (4) manually-operated globe valves, (5) manually-operated ball or plug valves, (6) check valves, (7) flexible hoses, (8) filters, (9) control valves (regulators), (10) relief valves, (11) liquid sensors, (12) pressure gages, and (13) differential pressure instruments. Smear, chemical compatibility, and mechanical tests were performed on 13 lubricants to determine their suitability for use with storable propellants. Additional safety information, practices, and procedures acquired during the pre-qualification test program are presented to amplify the safety practices outlined in AFBMDTN-61-32 (AD-255 145).
Author: United States. Dept. of Commerce. Office of Technical Services
Publisher:
ISBN:
Category :
Languages : en
Pages : 850
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Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Lubrication and lubricants
Languages : en
Pages : 256
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Author: United States. Dept. of Commerce. Office of Technical Services
Publisher:
ISBN:
Category :
Languages : en
Pages : 508
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Book Description
