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Rocket Motor

NSN: 1337-01-145-1963 | Model: 639AS4993
ITAR Registered seal

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.

NSN Properties and Flags
NATO Stock Number
1337-01-145-1963
DEMIL
Yes - ITAR Controlled (Code G)
Overall Length
70.000 inches
Specific Usage Design
Aim-9l/m, and natm-9l/m guided missile
Model Number
Mk36 mod 11
Motor Propellant Material
X61
Motor Propellant Grain Weight
60.0 pounds
Propellant Inhibitor
Not included
Igniter
Included
Igniter Installation
Installed
Igniter Model Number
Mk297 mod 1
Straight Section Outside Diameter
5.000 inches
Resonance Rod
Not included
Cubic Measure
0.3182 cubic feet
Package Reference Number
Mk287 mod 1 us navy
Dod Ammunition Code
1337-v888
Dot Registration Code
Ex1988090230
Special Features
Capture t handle
Gross Weight
129.0 shipping container pounds
Hazardous Material Classification Code
1.3 department of defense hazard class division
Quantity Per Shipping Container
1
Weight
99.00 pounds
Fsc Application Data
Guided missile
Reference Number Differentiating Characteristics
As differentiated by unit package quantity, unit package type, package model number, special features

Pricing and Availability

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NSN 1337-01-145-1963 Datasheet

Supply Class (FSC):
Solid Fuel; And Components Guided Missile And Space Vehicle Explosive Propulsion Units
Cross Reference:
  • 639AS4993
  • 1337-V888
Cage Codes:
  • Naval Air Systems Command (CAGE 30003)
  • Department Of Defense Ammunition (CAGE 99999)
Schedule B & Trade:
  • Schedule B: 9306900060 (NAICS 336415)

    Parts for guided missiles

  • SITC: 89129

    Munitions of war and parts thereof, n.E.S.

  • End Use: 50050

    Tanks, artillery, missiles, rockets, guns and ammunition

Identification:
HMIC

Y - Indicates information is in the hazardous materials information resource system (hmirs).

PMIC

A - Item does not contain precious metal.

ADPE

- Represents items with no adp components

CRITL

- The item does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application.

NSN Management Codes:
  • SOS
    Ncb
  • AAC
    C
  • Quantity per pack
    1
  • Unit of Measure
    Ea
  • Shelf Life
    N/A
  • Classification Control
    7
  • MGMT_CTL
    8e--bv-
  • Repariability
    Material (expendable ordnance) requiring lot number reporting

Questions & Answers:

What are the historical prices recorded for this stock number?
Historical data shows pricing from $26,968.50 to $44,947.50..
Does NSN 1337-01-145-1963 have a shelf life?
No. There is no shelf life applicable for this NSN.
What NATO entities are users of this NSN?
Department Of The Air Force, Department Of The Navy, Nadb (nato Ammunition Data Base), Czech Republic, Singapore, Australia, Belgium, Canada, New Zealand, Germany, Republic Of Korea, Netherlands, Greece, Turkey, and Nato Maintenance and Supply Agency
What is the NIIN of NSN 1337-01-145-1963?
011451963 or 01-145-1963
Does NSN 1337-01-145-1963 require demilitarization?
Yes - ITAR Controlled
What is the most recent solicitation for NSN 1337-01-145-1963?
No solicitations for this NSN.
When was this national stock number assigned to the federal catalog?
Jan 07, 1983
MSDS

Material Safety

MSDS CCGKN 1337-V888 MK 36 ROCKET MOTOR; TX 683 TPH 8288

Hazards

Routes of entry: inhalation: yes skin: no ingestion: no
reports of carcinogenicity: ntp: no iarc: no osha: no
health hazards acute and chronic: inhalation: decomposition could cause
respiratory damage. Eyes: decomposition extremely irritating.

explanation of carcinogenicity: none
effects of overexposure: breathing difficulty, irritation.

First Aid

First aid: inhalation: remove to fresh air. Eyes: flush w/large amounts
of water for 15 mins. Obtain medical attention in all cases.

Chemical Properties

Appearance and odor: rubbery/solid/grey propellant in an aluminum
case/nozzle w/slight aromatic odor

Reactivity

Stability indicator/materials to avoid: no
strong acids, alkalies.

stability condition to avoid: temps >200f, shock, impact, friction &
static charge buildup.

hazardous decomposition products: co2, co, hydrogen chloride, hydrogen
oxide, nitrogen oxide.

Proper Disposal

Waste disposal methods: fired motors are non-hazardous & may be disposed
of iaw/federal, state & local regulations.

disclaimer (provided with this information by the compiling agencies):
this information is formulated for use by elements of the department
of defense. the united states of america in no manner whatsoever,
expressly or implied, warrants this information to be accurate and
disclaims all liability for its use. any person utilizing this
document should seek competent professional advice to verify and
assume responsibility for the suitability of this information to their
particular situation.

Ingredients List

Ingred name: ammonium perchlorate
cas: 7790-98-9
rtecs #: sc7520000

ingred name: adipic acid, bis(3-cyclohexenylmethyl) ester; adipic acid,
3-cyclohexenylmethanol diester *96-3*
cas: 63905-29-3
rtecs #: au8925000

ingred name: hx 752

ingred name: hydroxyl terminated polybutadiene

ingred name: cyclonite; s-triazine; hexahydro 1,3,5-trinitro;
cyclotrimethylenetrinitramine (rdx)
cas: 121-82-4
rtecs #: xy9450000
acgih tlv: 1.5 mg/cum (skin)

ingred name: zirconium carbide
cas: 12070-14-3

ingred name: aramid fiber

ingred name: amorphous silica, amorphous-diatomaceous earth
cas: 61790-53-2
rtecs #: hl8600000
other rec limits: 20 mccpf (msha)
acgih tlv: 10 mg/cum dust

ingred name: polyisophrene rubber

ingred name: boron potassium nitrate

ingred name: ammonium perchlorate
cas: 7790-98-9
rtecs #: sc7520000

ingred name: catocene

ingred name: isophorone diisocyanate
cas: 4098-71-9
rtecs #: nq9370000
other rec limits: 0.005 ppm
acgih tlv: 0.045 mg/cum (skin)

ingred name: phenolic glass