1340-J104

Rocket Motor

NSN 1340-00-157-6949

DEMIL
Shelf Life
UOM
NIIN
Demil:
DEMIL/MLI
Shelf Life:
UOM:
NIIN:
001576949

Technical Specifications of NSN

Overall Length:
39.340 inches
Size Designation:
2.75 inch
Specific Usage Design:
2.75 in. Rocket
Motor Propellant Grain Quantity:
1
Motor Propellant Material:
Ammonium perchlorate-polysulfide
Motor Propellant Grain Model Number:
1148155-1
Motor Propellant Grain Weight:
8.3 pounds
Propellant Inhibitor:
Not included
Igniter:
Included
Igniter Installation:
Installed
Propellant Accommodation Type:
Solid
Straight Section Outside Diameter:
2.750 inches
Integral Stabilization Method:
Fin
Criticality Code Justification:
Exwt
Dod Ammunition Code:
1340-j104
Dot Registration Code:
Ex1988090247
Net Explosive Weight:
8.3 storage pounds and 8.3 transportation pounds
Gross Weight:
131.0 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:
6
NSN:
1340-00-157-6949
Item Name:
Engine,rocket,solid Propellant
Cage Code:
99999

Other Related Parts

Part Number
Cage
RNCC
RNVC
RNAAC
Status
MSDS
SADC
Part Number:
SR105AJ1
Cage Code:
07878
RNCC:
5
RNVC:
1
RNAAC:
SU
Status:
A
MSDS:
SADC:
Part Number:
1148178
Cage Code:
05824
RNCC:
3
RNVC:
2
RNAAC:
SU
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:
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:
ZZ
LVL_A:
LVL_B:

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
064300
UFC:
05980
LTL:
200.0
LCL:
--
WCC:
427
TCC:
J
SHC:
9
ACC:
Ammunition

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Pricing & Availability

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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:
NADB (NATO AMMUNITION DATA BASE) Nadb (nato Ammunition Data Base)
DSOR:
Import / Export
  • Schedule B: 9306900080
  • SITC: 89129
  • End Use: Tanks, artillery, missiles, rockets, guns and ammunition
  • NAICS: 332993
  • USDA: 1

Classification: Parts for bombs, grenades, torpedos, mines, and similar munitions of war


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