A114301

Rocket Motor

NSN 1377-01-255-1650

DEMIL
Shelf Life
UOM
NIIN
Demil:
DEMIL/MLI
Shelf Life:
N/A
UOM:
1 EA
NIIN:
012551650

Detail Specifications

Overall Length:
14.125 inches
End Application:
F-16, f-15, f10, b-1b acft
Size Designation:
Any acceptable
Propellant Inhibitor:
Not included
Igniter:
Not included
Nozzle Cant Angle In Deg:
51.0
Resonance Rod:
Not included
Criticality Code Justification:
Exwt
Dod Ammunition Code:
1377-mt32
Dot Identification Number:
Un0186
Dot Registration Code:
Ex1988080414
Net Explosive Weight:
1.1 storage pounds and 1.1 transportation pounds
Dot Hazard Class/division:
1.3
Hazardous Material Classification Code:
1.3 department of defense hazard class division
Dot Proper Shipping Name:
Rocket motors
Dot Warning Label Code:
1.3c
NSN:
1377-01-255-1650
Item Name:
Engine,rocket,solid Propellant
Cage Code:
88277

Manufacturer Part Numbers

Part Number
Cage
RNCC
RNVC
RNAAC
Status
MSDS
SADC
Part Number:
50436-11
Cage Code:
12116
RNCC:
3
RNVC:
2
RNAAC:
ME
Status:
A
MSDS:
SADC:
Part Number:
1377-MT32
Cage Code:
99999
RNCC:
6
RNVC:
9
RNAAC:
ME
Status:
A
MSDS:
SADC:
Part Number:
1377PL1023165
Cage Code:
9009H
RNCC:
5
RNVC:
9
RNAAC:
9Z
Status:
A
MSDS:
SADC:

Part Identification

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
21790
FIIG:
T357-B
Concept No.:
App. Key:
BA
Cond. Code:
2
Status:
A

Part Materials

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
Y
PMIC:
A
ESD:
ESD:
MMAC:
ES
CRITL:
F

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
19.3 X 7.3 X 7.0
Paclk Weight:
16.0000lbs
Item Weight:
3.5000lbs
Item Dim:
014100220022
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
A
SPI No.:
F001192033
SPI Rev.:
N
SPC Mkg:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
064300
UFC:
05980
LTL:
200.0
LCL:
85.0
WCC:
404
TCC:
J
SHC:
9
ACC:
Explosives

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Privacy | Terms

Definition Definition of approved item name (AIN): "Solid Propellant Rocket Engine"

A nonairbreathing reaction propulsion device that consists essentially of a thrust chamber and exhaust nozzle, and that carries its own solid oxidizer-fuel combination from which hot gases are generated by combustion and expanded through a nozzle. See also rocket motor cluster.

MOE Major Organizational Entities

Entity
DSOR
User:
DEPARTMENT OF THE AIR FORCE Dept. of the Air Force
DSOR:
FH
User:
DEPARTMENT OF THE NAVY Dept. of the Navy
DSOR:
FH
User:
NADB (NATO AMMUNITION DATA BASE) Nadb (nato Ammunition Data Base)
DSOR:
User:
POLAND Poland
DSOR:
User:
SINGAPORE Singapore
DSOR:
User:
BELGIUM Belgium
DSOR:
User:
REPUBLIC OF KOREA Republic of Korea
DSOR:
User:
NETHERLANDS Netherlands
DSOR:
User:
PORTUGAL Portugal
DSOR:
User:
DENMARK Denmark
DSOR:
User:
NORWAY Norway
DSOR:
User:
GREECE Greece
DSOR:
User:
TURKEY Turkey
DSOR:
Import / Export
  • Schedule B: 9306900060
  • SITC: 89129
  • End Use: Tanks, artillery, missiles, rockets, guns and ammunition
  • NAICS: 336415
  • USDA: 1

Classification: Parts for guided missiles


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