Jump to content

Dervish (rocket)

From Wikipedia, the free encyclopedia
Dervish
TypeUnguided rocket
Place of originUnited States
Production history
Designed1950s
ManufacturerNorthrop Corporation
Specifications
Diameter2.75 inches (70 mm)

EngineThiokol TRX-126B
PropellantSolid fuel
Guidance
system
Unguided

Dervishwas an unguidedair-to-airandair-to-surface rocketdeveloped by theNorthrop Corporationfor use by theUnited States NavyandUnited States Armyduring the early 1950s. Originally intended as an air-to-air rocket to replace theMighty Mouserocket, it was later expanded in role to also operate in an air-to-surface capacity.[1]Spin-stabilized, 2.75 inches (70 mm) in diameter, and powered by aThiokolTRX-126Bsolid fuel rocket,[2]in 1958 development of Dervish was resumed as a solely Army project, but no production ever emerged.[3][4]

References

[edit]

Citations

[edit]
  1. ^Ordway and Wakeford 1960, p.31
  2. ^Aviation Week & Space Technology,volume 69 (1958), p.61
  3. ^Aircraft and Missiles Manufacturing,Volume 2 (1959), p.28
  4. ^Jacobs and Whitney 1962, p.46

Bibliography

[edit]
  • Jacobs, Horace; Eunice Engelke Whitney (1962).Missile and Space Projects Guide 1962.New York: Springer Science+Business Media.ISBN978-1-4899-6967-5.
  • Ordway, Frederick Ira & Wakeford, Ronald C. (1960).International Missile and Spacecraft Guide.New York: McGraw-Hill.ASINB000MAEGVC.