LTV-N-4

Last updated
LTV-N-4
LTV-N-4 rocket at NOTC Inyokern in 1949.jpg
Type Experimental rocket
Place of origin United States
Service history
In service 1949
Used by United States Navy
Production history
Designer Naval Ordnance Test Station
Specifications
Length 15 feet (4.6 m)

Engine Solid-fuel rocket

The LTV-N-4 was an American experimental rocket, developed by the Naval Ordnance Test Station for the development and testing of large solid-fueled rocket boosters for ramjet-powered missiles. Described as "more powerful than the V-2", a number of test flights were conducted during 1949. [1] [2]

Ramjet jet engine that uses the engines forward motion to compress incoming air

A ramjet, sometimes referred to as a flying stovepipe or an athodyd, is a form of airbreathing jet engine that uses the engine's forward motion to compress incoming air without an axial compressor or a centrifugal compressor. Because ramjets cannot produce thrust at zero airspeed, they cannot move an aircraft from a standstill. A ramjet-powered vehicle, therefore, requires an assisted take-off like a rocket assist to accelerate it to a speed where it begins to produce thrust. Ramjets work most efficiently at supersonic speeds around Mach 3. This type of engine can operate up to speeds of Mach 6.

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References

Citations
  1. Parsch 2003
  2. Bowman 1957, p.149.
Bibliography

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