Ping-Pong (rocket)

Reconnaissance missile From Wikipedia, the free encyclopedia

Ping-Pong was a battlefield reconnaissance rocket developed by Lockheed-California – later the Lockheed Missiles and Space Company – for use by the United States Army. Intended to give battlefield commanders the ability to gain photographic data on enemy locations, it reached the flight-test stage before being cancelled.

TypeReconnaissance missile
PlaceoforiginUnited States
Quick facts Type, Place of origin ...
Ping-Pong
TypeReconnaissance missile
Place of originUnited States
Service history
Used byUnited States Army
Production history
DesignerLockheed Missiles and Space Company
Designed1964
Specifications
WarheadCameras

EngineRocket
PropellantSolid fuel
Guidance
system
Ballistic
Close

Development history

In 1964, the United States Army called for proposals for a rocket that could be launched by Army units towards the suspected location of enemy units, with a camera carried on board the rocket taking pictures of the target area, before a second retrorocket motor, located in the nose of the rocket, fired to return it to its point of launch for analysis of its reconnaissance pictures.[1] Proposals were received from Lockheed-California, Goodyear Aerospace, the Chrysler Corporation Missile Division, and Beech Aircraft; the Lockheed proposal, named "Ping-Pong", was funded for development.[2]

Ping-Pong was conventional in appearance, launched from a tube 4 inches (100 mm) in diameter.[3] A cruciform fin arrangement provided stabilization; the fins were mounted on a sliding assembly, allowing them to shift to the opposite end of the rocket's body when the retrorocket was fired to reverse the rocket's direction for the return flight.[1]

Flight testing of Ping-Pong took place at Rosamond Dry Lake in California during the second half of 1964.[1] The tests were considered to be successful,[4] with the rocket being reported as "the free world's only round-trip ballistic missile";[5] however, follow-up studies did not result in further development.[3]

References

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