802691

Rocket Motor

NSN 1337-00-908-6852

DEMIL
Shelf Life
UOM
NIIN
Demil:
DEMIL/MLI
Shelf Life:
N/A
UOM:
EA
NIIN:
009086852

Technical Specifications of NSN

End Application:
Aim-7e guided missile
Motor Propellant Grain Model Number:
Mk 75 mod 1
Motor Propellant Grain Weight:
91.6 pounds
Criticality Code Justification:
Exwt
Dod Ammunition Code:
1337-v343
Dot Registration Code:
Ex1988060885
Net Explosive Weight:
91.599998 storage pounds and 91.599998 transportation pounds
Gross Weight:
1681.0 pallet pounds and 264.6 shipping container pounds
Dot Hazard Class/division:
1.3
Hazardous Material Classification Code:
1.3 department of defense hazard class division
Quantity Per Shipping Container:
1
NSN:
1337-00-908-6852
Item Name:
Rocket Motor,grain Loaded
Cage Code:
00405

Other Related Parts

Part Number
Cage
RNCC
RNVC
RNAAC
Status
MSDS
SADC
Part Number:
LD624129
Cage Code:
10001
RNCC:
3
RNVC:
2
RNAAC:
JG
Status:
A
MSDS:
SADC:
Part Number:
2546916
Cage Code:
10001
RNCC:
5
RNVC:
2
RNAAC:
JG
Status:
A
MSDS:
SADC:
Part Number:
1337-V343
Cage Code:
99999
RNCC:
6
RNVC:
9
RNAAC:
SB
Status:
A
MSDS:
SADC:
Part Number:
802691
Cage Code:
0MVU3
RNCC:
C
RNVC:
1
RNAAC:
ZZ
Status:
A
MSDS:
SADC:
9F

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:
U
ESD:
ESD:
MMAC:
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
9,999.9000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
M
SPI No.:
SPI Rev.:
SPC Mkg:
03
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
064300
UFC:
05980
LTL:
200.0
LCL:
--
WCC:
417
TCC:
J
SHC:
9
ACC:
Explosives

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Pricing & Availability

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Definition Definition of approved item name (AIN): "Grain Loaded Rocket Motor"

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:
NADB (NATO AMMUNITION DATA BASE) Nadb (nato Ammunition Data Base)
DSOR:
User:
REPUBLIC OF KOREA Republic of Korea
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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