Author:
Publisher:
ISBN:
Category : Handbooks, manuals, etc
Languages : en
Pages : 164
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.
Titan II Storable Propellant Handbook
Author:
Publisher:
ISBN:
Category : Handbooks, manuals, etc
Languages : en
Pages : 164
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.
Publisher:
ISBN:
Category : Handbooks, manuals, etc
Languages : en
Pages : 164
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.
TITAN II STORABLE PROPELLANT HANDBOOK (Final Handbook Revision B).
Titan Ii Storable Propellant Handbook. Final Handbook
Author: RALPH R. LIBERTO
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
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).
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
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).
Storable Propellant Data for the Titan II Program
Author: Ralph R. Liberto
Publisher:
ISBN:
Category : Matter
Languages : en
Pages : 86
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).
Publisher:
ISBN:
Category : Matter
Languages : en
Pages : 86
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).
Storable Liquid Propellants for Titan II
Author: Aerojet-General Corporation. Liquid Rocket Plant
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages :
Book Description
Compatibility of Materials with Rocket Propellants and Oxidizers
Author: Walter K. Boyd
Publisher:
ISBN:
Category : Liquid propellants
Languages : en
Pages : 46
Book Description
The memorandum summarizes the available information on the compatibility of liquid rocket propellants with prominent materials of construction. Fuels and oxidizers of current interest are discussed. The corrosion data which are presented will apply to storing, handling, and control equipment outside of missiles and to missile components excluding combustion chamber. The compatibility of materials with reaction products in combustion chambers, nozzles, etc., is not considered. Included in the summary are data for many nonmetallic materials. The memorandum is subdivided into sections according to the propellant. Each material of construction is rated for a given medium as belonging to one of four classes, based primarily upon corrosion resistance. Consideration also is given to such factors as catalytic decomposition and sensitivity to impact.
Publisher:
ISBN:
Category : Liquid propellants
Languages : en
Pages : 46
Book Description
The memorandum summarizes the available information on the compatibility of liquid rocket propellants with prominent materials of construction. Fuels and oxidizers of current interest are discussed. The corrosion data which are presented will apply to storing, handling, and control equipment outside of missiles and to missile components excluding combustion chamber. The compatibility of materials with reaction products in combustion chambers, nozzles, etc., is not considered. Included in the summary are data for many nonmetallic materials. The memorandum is subdivided into sections according to the propellant. Each material of construction is rated for a given medium as belonging to one of four classes, based primarily upon corrosion resistance. Consideration also is given to such factors as catalytic decomposition and sensitivity to impact.
Handbooks
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 136
Book Description
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 136
Book Description
Pressurization Systems Design Guide: Pressurant gas solubility in liquid propellants
Author: Aerojet-General Corporation
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 232
Book Description
Publisher:
ISBN:
Category : Rocket engines
Languages : en
Pages : 232
Book Description
Additional Information and Data Pertaining to the Installation and Operation of a Storable Propellant Facility for Testing of Titan II Components and Systems
High Energy Propellants
Author:
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 86
Book Description
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 86
Book Description