10230201-504

Rocket Motor Exhaust Nozzle

NSN 1338-01-234-7485

DEMIL

Shelf Life

UOM

NIIN

Demil:

DEMIL/MLI

Shelf Life:

N/A

UOM:

1 EA

NIIN:

012347485

Product Technical Spec.

End Application:

1410-01-205-7066

Test Data Document:

18876-10230201-504 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing)

General Description:

18.076 in l; 11.067 in d; beveled to 5.687 in d on thrust end

NSN:

1338-01-234-7485

Item Name:

Nozzle,exhaust,rocket Motor

Cage Code:

02266

Cross Referenced Parts

Part Number

Cage

RNCC

RNVC

RNAAC

Status

MSDS

SADC

Part Number:

10230201-504

Cage Code:

18876

RNCC:

RNVC:

RNAAC:

Status:

MSDS:

SADC:

Part Identification

INC

FIIG

Concept No.

App. Key

Cond. Code

Status

INC:

22411

FIIG:

A23900

Concept No.:

App. Key:

Cond. Code:

Status:

Part Materials

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators

HMIC

PMIC

ESD/EMI

ENAC

MMAC

CRITL

HMIC:

PMIC:

ESD:

MMAC:

CRITL:

Packaging & Shipping

Est. Pack Size

Est. Pack Weight

Est. Item Weight

Est. Item Dim.

Pack Size:

18.0 X 18.0 X 24.6

Paclk Weight:

44.9000lbs

Item Weight:

13.6000lbs

Item Dim:

018101110111

OPI

SPI No.

SPI Rev.

SPC Mkg.

LVL A

LVL B

OPI:

SPI No.:

SPI Rev.:

SPC Mkg:

LVL_A:

LVL_B:

Freight Classification

NMFC

UFC

LTL

LCL

WCC

TCC

SHC

ACC

NMFC:

162812

UFC:

73210

LTL:

85.0

LCL:

85.0

WCC:

686

TCC:

SHC:

ACC:

Equipment for Aircraft

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 10230201-504 and/or cross reference parts.

Definition Definition of approved item name (AIN): "Rocket Motor Exhaust Nozzle"

An item designed with a constricting throat section and a divergent section. The constricting throat section compresses the propellant gases and maintains the pressure within the thrust chamber of the rocket motor by limiting the flow of gases. The divergent section controls the expansion of the gases causing increased thrust.