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MIL-PRF-7254G

PROPELLANT, NITRIC ACID

Organization:
AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering)
Year: 1997

Abstract: This specification covers the requirements for four types of nitric acid propellant.
The nitric acid will be of the following types as specified (6.2):
The types of nitric acid are as follows:
     Type IIIA  - Nominal 14 percent NO2 content plus corrosion inhibitor       Type IIIB  - Nominal 14 percent NO2 content, lower solids content, plus                   corrosion inhibitor       Type IIILS - Limited storage propellant with nominal 14 percent NO2                   content, lower solids content, plus corrosion inhibitor, and                   limited iron content       Type IV    - High density propellant with nominal 44 percent NO2 content,                   lower solids content, plus corrosion inhibitor, and limited                   iron content


Intended Use: The propellants covered by this specification are intended for use as oxidizers in rocket engines. Type IIILS is intended for special purposes and will not be used for applications where storage life is a criterion because of its tendency to change composition.
URI: https://yse.yabesh.ir/std/handle/yse/229854
Subject: Hydrofluoric acid
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    MIL-PRF-7254G

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contributor authorAIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering)
date accessioned2017-09-04T18:48:33Z
date available2017-09-04T18:48:33Z
date copyright35779
date issued1997
identifier otherKPHBEAAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/229854
description abstractThis specification covers the requirements for four types of nitric acid propellant.
The nitric acid will be of the following types as specified (6.2):
The types of nitric acid are as follows:
     Type IIIA  - Nominal 14 percent NO2 content plus corrosion inhibitor       Type IIIB  - Nominal 14 percent NO2 content, lower solids content, plus                   corrosion inhibitor       Type IIILS - Limited storage propellant with nominal 14 percent NO2                   content, lower solids content, plus corrosion inhibitor, and                   limited iron content       Type IV    - High density propellant with nominal 44 percent NO2 content,                   lower solids content, plus corrosion inhibitor, and limited                   iron content


Intended Use: The propellants covered by this specification are intended for use as oxidizers in rocket engines. Type IIILS is intended for special purposes and will not be used for applications where storage life is a criterion because of its tendency to change composition.
languageEnglish
titleMIL-PRF-7254Gnum
titlePROPELLANT, NITRIC ACIDen
typestandard
page17
statusActive
treeAIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering):;1997
contenttypefulltext
subject keywordsHydrofluoric acid
subject keywordsIRFNA
subject keywordsMissile propellant
subject keywordsNitric acid
subject keywordsNitrogen dioxide
subject keywordsOxidizer
subject keywordsRocket engines
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