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MIL-STD-815A.009125.PDF
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MIL-STD-815A.009125.PDF
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MIL-STD-815A(USAF)
30 September 1~0
Superseding
MIL-STD-81;(USAF)
14 June 1962
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MILITARY STANDARD
TYFS DESIGNATION SYSTEM FOR RCCKET ENGINES, MOTORS
AND HYSRIDS
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MIL-STD-815A(USAF)
30 September 1~0
DEPAR’f?fEIWOF THE AIR FORCE
AIR FORCE SYSTEMSCOMMAND
AIR FORCE ROXtT PROPULSIONLABORATORY
Type DesignationSystem for RocketEngines,Motors end Hybrids
ML-STD-815A(USAF)
1. This Military Stsnderdwas approved30 September1~0 and
is mandatoryfor use by the Departmentof the Air Force.
2. Recommendedcorrections,additions,or deletionsshouldbe
addressedto:
Air Force Rocket PropulsionLaborato~ (FWOIS),
Edwards,California93523.
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MIL-STD-815A(USAF)
30 September1~0
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FOREWOSD
The purpose of this standardis to providea type designation
system,and uniformproceduresfor type designationand item ident-
ificationin accordancewith MIL-STD-842(USAF). The systemas
identifiedherein has been developedto standardizethe identification
of rocket engines, motors, snd hybrids as used by the Air Force.
Frotisionshave been protidedin the standsrdfor its use by the other
Defense Departmentswhen appropriate.
The type designationsystem as defined herein for rocket engines
was adopted25 June 1958 for the Departmentof the Air Force and the
Departmentof the Navy, Bureau of Aeronauticsuse as Air Force-Navy
AeronauticalBulletin352.
Similsrly,the designationsystem as de-
fined herein for rocketmotors (then known as jet thrust unit6) was
adopted 22 July 1948 as Air Force-NavyAeronauticalEulletin353. This
stsndsrdwas developedby the Air Force snd approved
14 June 1962 to
meet military standardfommt as prescribedby standardizationpolicy.
It modernizesand expandsthe designationsystemsof ANA Bulletins352
end 353 to providean improvedtype designationfor modern and future
rocket propulsionsystems.
!Fnisstsnderdis intendedto serve as an authoritativeguide for
Air Force activitiesand associatedcontractorswho preparencunenclature
requestsfor rocket engines,motnrs and hybridsdesignations.
Included
are instructionsto insure that request forms are properlycompleted,
that the proper number of requestsare submitted,and the routingthat
shouldbe followed.
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