Jaguar (American rocket)

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ManufacturerARDC
Country of originUnited States
Height8.029 m (26 ft 4.1 in)
Jaguar
Jaguar in front of B-57 launch aircraft
FunctionSounding rocket
ManufacturerARDC
Country of originUnited States
Size
Height8.029 m (26 ft 4.1 in)
Diameter0.53 m (21 in)
Mass730 kg (1,600 lb)
StagesThree
Payload to 800 km (500 mi)
Mass16 kg (35 lb)
Launch history
StatusRetired
Launch sitesWhite Sands
Total launches2
First flight1960
Last flight1961
First stage – Recruit cluster
Diameter0.53 m (21 in)
Powered by3 x XM19
Maximum thrust156 kN (35,000 lbf) each
Burn time1.5 s
Propellantsolid
Second stage – Recruit
Diameter23 cm (9 in)
Powered by1 x XM19
Maximum thrust156 kN (35,000 lbf)
Burn time1.5 s
Propellantsolid
Third stage – Baby Sergeant
Diameter16 cm (6.4 in)
Powered by1 x 5.4KS1975
Maximum thrust8.8 kN (2,000 lbf)
Burn time5.4 s
Propellantsolid

Jaguar was a three-stage sounding rocket developed by the United States Air Force in the early 1960s.[1] Designed for air launch to allow soundings from remote areas without infrastructure, it was only launched twice before the project was abandoned.

Jaguar was an air-launched sounding rocket developed by the Air Research and Development Command of the U.S. Air Force, intended for use for high-altitude scientific research into the aurora borealis and radiation trapped in the Van Allen Belts.[2] Derived from a design used by the Lewis Flight Propulsion Laboratory,[2] it was a three-stage vehicle, with a first stage of three clustered Recruit rockets, a single Recruit as a second stage,[3] and a third stage with a Baby Sergeant rocket.[2][1] It was to be launched using a Martin B-57 Canberra medium bomber that was modified to carry the rocket on a side-mounted pylon; this allowed for the rocket to be launched from any location capable of operating a jet aircraft, without the need for installing launch infrastructure in remote areas.[4] To launch, the Canberra would pull into a near-vertical climb, akin to that used for toss bombing, and release the rocket;[2] Jaguar was expected to be capable of launching a 16-kilogram (35 lb) payload to an apogee of 800 kilometres (500 mi).[3] An upgraded version using the improved "Yardbird" model of the Recruit was proposed.[5]

Operational history

See also

References

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