1340-H305

Rocket Motor

NSN 1340-00-028-6133

DEMIL
Shelf Life
UOM
NIIN
Demil:
DEMIL/MLI
Shelf Life:
UOM:
NIIN:
000286133

Detail Specifications

Overall Length:
21.500 inches
Model Number:
M3
Motor Propellant Grain Quantity:
7
Motor Propellant Material:
Ballistite
Motor Propellant Grain Model Number:
M16
Motor Propellant Grain Weight:
9.17 pounds
Cable Assembly Model Number:
Not assigned
Propellant Inhibitor:
Not included
Igniter:
Included
Igniter Installation:
Installed
Propellant Accommodation Type:
Extruded double-base solid
Igniter Model Number:
M21
Cable Assembly Connector Type:
Two-prong special
Burning Time In Seconds:
0.70
Thrust:
2650.000 pounds
Straight Section Outside Diameter:
5.120 inches
Resonance Rod:
Not included
Dod Ammunition Code:
1340-h305
Weight:
17.93 pounds
NSN:
1340-00-028-6133
Item Name:
Engine,rocket,solid Propellant
Cage Code:
99999

Manufacturer Part Numbers

Part Number
Cage
RNCC
RNVC
RNAAC
Status
MSDS
SADC
Part Number:
MILJ12823
Cage Code:
81349
RNCC:
5
RNVC:
1
RNAAC:
JG
Status:
A
MSDS:
SADC:
Part Number:
82-6-24
Cage Code:
19203
RNCC:
3
RNVC:
2
RNAAC:
BF
Status:
A
MSDS:
SADC:
Part Number:
ES2650
Cage Code:
18876
RNCC:
5
RNVC:
2
RNAAC:
BD
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:
N
PMIC:
A
ESD:
ESD:
MMAC:
CRITL:
X

  We Guarantee with Every Order

  •   100% Genuine Manufacturers Parts
  •   Every Product thoroughly Inspected
  •   Sales Record Retention of 7 years
  •   Fast Delivery
  •   HAZMAT Certified
  •   Global Shipping

Pricing & Availability

Submit this form for current pricing and availability quote on part number 1340-h305 and/or cross reference parts.
Part / NSN:
Qty:
Your Email:
Phone:
Ref. / PO #:
Company:

We do not share or sell your information to anyone.
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:
User:
NATO MAINTENANCE AND SUPPLY AGENCY NATO Maintenance and Supply Agency
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


Best-Selling Products A collection of our most popular products