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Inertial Guidance System, Poseidon C-3

Air and Space Museum

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International media Interoperability Framework
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Object Details

Model Maker

Exhibits of California, Inc.

Manufacturer

MIT Instrumentation Laboratory

Manufactured for

United States Navy

Summary

This is part of the inertial guidance system of a U.S. Navy Poseidon C-3 submarine-launched ballistic missile (SLBM). Designed by the MIT Instrumentation Laboratory, it used a set of gyroscopes and accelerometers to measure the missile's velocity and position.
Developed by Lockheed, Poseidon C-3s were two-stage, solid-fuel missiles with a range of approximately 5300 km (3,300 miles). Deployed from 1971 to the early 1990s, sixteen missiles were carried on a submarine, with each missile having up to 16 independently-targetable nuclear warheads.
This specimen was made from spare parts and donated by the U.S. Navy to the Museum in 1973.

Credit Line

Transferred from Lockheed Missiles & Space Company

Inventory Number

A19731668002

Restrictions & Rights

Usage conditions apply

Type

CRAFT-Missile & Rocket Parts

Materials

Wood, metal, and plastic

Dimensions

Other (MK3): 2 ft. tall x 1 ft. 6 in. wide (60.96 x 45.72cm)

Country of Origin

United States of America

See more items in

National Air and Space Museum Collection

Location

Steven F. Udvar-Hazy Center in Chantilly, VA

Exhibit Station

Rockets & Missiles

Data Source

National Air and Space Museum

Metadata Usage

Not determined

Link to Original Record

http://n2t.net/ark:/65665/nv9bb027d72-8055-461c-a1a0-81c5256115c7

Record ID

nasm_A19731668002

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