1340000388217

ROCKET MOTOR

Part No.: 3-1,1340-J102,J2757010310,J30501031,

NSN Summary
NSN Description Assign Criticality Status Codification Country
1340000388217 ROCKET MOTOR 01/01/1963 X Inactive

Open Solicitations

Issued Closing Solicitation Clin Cage ECV Status

Request A Demo

Request a Demo to see all details.

Request Demo

Manufacturers

Part Number Company Cage P/N added P/N deleted RNVC RNCC RNAAC RNFC SADC DAC Item Status
3-1 ######### ######### ######### ######### ######### ######### ######### ######### ######### ######### #########
1340-J102 ######### ######### ######### ######### ######### ######### ######### ######### ######### ######### #########
J2757010310 ######### ######### ######### ######### ######### ######### ######### ######### ######### ######### #########
J30501031 ######### ######### ######### ######### ######### ######### ######### ######### ######### ######### #########

Request A Demo

Request a Demo to see all details.

Procurement History

Company Cage Award Date Qty Unit Price Total Price Contract Delivery

Request A Demo

Request a Demo to see all details.

Request Demo

Management Data

MOE SOS AAC Unit Pack UOM Unit Price SLC Date ELA FCS MCC

Technical Info

Name Value
STRAIGHT SECTION OUTSIDE DIAMETER 2.750 INCHES NOMINAL
NOMINAL THRUST 7.200 POUNDS
RESONANCE ROD INCLUDED
MODEL NUMBER MK 3 MOD 1
OVERALL LENGTH 39.920 INCHES NOMINAL
SIZE DESIGNATION 2.75 INCH
PROPELLANT INHIBITOR INCLUDED
IGNITER INCLUDED
CABLE ASSEMBLY MODEL NUMBER NOT ASSIGNED
MOTOR PROPELLANT GRAIN WEIGHT 6.4 POUNDS
REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS AS DIFFERENTIATED BY UNIT PACKAGE QUANTITY,UNIT PACKAGE TYPE,PACKAGE MODEL NUMBER
MOTOR PROPELLANT GRAIN MODEL NUMBER MK 43 MOD 1
PROPELLANT ACCOMMODATION TYPE EXTRUDED CYLINDER SOLID W/INTERNAL STAR-SHAPED LONGITUDINAL CAVITY
CABLE ASSEMBLY CONNECTOR TYPE INTEGRAL CONTACT
IGNITER MODEL NUMBER MK 125 MOD 4
INTEGRAL STABILIZATION METHOD FIN
MOTOR PROPELLANT GRAIN QUANTITY 1
MOTOR PROPELLANT MATERIAL BALLISTITE
DOD AMMUNITION CODE 1340-J102
WEIGHT 6.22 POUNDS
NOMINAL BURNING TIME IN SECONDS 1.69
IGNITER INSTALLATION INSTALLED

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.


FIIG Inc Info

FIIG INC Description Detail
21790 21790 ROCKET MOTOR

MOE Data

Country MOE AMC AMSC NIMSC Eff Date IMC IMCA DSOR Collaborator Receiver AAC FMOE

Freight Data

Integrity Originating HMC WCC TCC SHC ADC ACC ASH LTL NMFC NMFC Sub Item UFC Freight Description Rail Variance
XX

Packaging Data

Source PICA / SICA Packaging Category Storage Preservation Clean/Dry INT Qty Unit Weight Unit Size Unit Pack Cube Item Weight Item Dims
Preservation Material Wrapping Material Cushioning / Dunnage Cushioning Thickness Unit Container Intermediate Container UCL Special Marking Level A Packing Level B Packing Minimal Packing Optional Procedure

Item Standardization

Status Code Originator Date Status
Not Standardized yet 98 02/01/1975 Inactive