AIA NAS3620
PROPELLANTS, NITROGEN TETROXIDE
Aerospace Industries Association , 05/31/2013
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The propellant described by this specification is intended for use as an oxidizer in rocket engines.
INACTIVE FOR NEW DESIGN * X-REF NAS380Purpose. This specification covers the requirements for three types of nitrogen tetroxide (N2O4) propellants with separate requirements for procurement and use
Product Information
Published:
05/31/2013
Pages:
32
File Size:
1 file , 2.2 MB
Language:
English
