AIA NAS3620
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PROPELLANTS, NITROGEN TETROXIDE
Aerospace Industries Association , 05/31/2013
Pages: 32
The propellant described by this specification is intended for use as an oxidizer in rocket engines.
INACTIVE FOR NEW DESIGN * X-REF NAS380
Purpose. This specification covers the requirements for three types of nitrogen tetroxide (N2O4) propellants with separate requirements for procurement and use
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