Sparoair

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File:Sparoair II.jpg
Sparoair II on F4D
FunctionSounding rocket
Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value).Naval Missile Center
Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value).United States
Size
Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value).3.68 m (12 ft 1 in)
Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value).200 mm (8 in)
Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value).143 kg (315 lb)
StagesTwo
Capacity
Payload to 120 km (65 nmi)
Lua error in Module:WikidataIB at line 555: attempt to index field 'wikibase' (a nil value).18 kg (40 lb)
Launch history
StatusRetired
Launch sitesPoint Mugu
Total launches>14
First flight1960
Last flight26 May 1966

Sparoair was a family of air-launched sounding rockets developed by the United States Navy in the late 1950s and early 1960s. Based on the Sparrow air-to-air missile, three versions of the rocket were developed;[1][2][3] all launches were from Point Mugu and although some were successful,[4][1][2][3] the system did not enter operational service.

Versions

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Sparoair I and II

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Sparoair was developed by the Naval Missile Center, as a two-stage development of the Sparrow III air-to-air missile.[5][6] Propelled by two Sparrow rocket motors mounted in tandem,[7] the Sparoair could be launched from F3H (F-3) Demon and F4D (F-6) Skyray fighter aircraft, and was capable of lifting a 40 pounds (18 kg) payload to an apogee of 65 nautical miles (120 km; 75 mi).[8][6]

The Sparoair I was the original version of the rocket, launched using an ejection system and a lanyard for firing; after that proved unreliable in flight testing, the Sparoair II was developed that utilised a rail launch with ignition prior to release from the aircraft.[5] Eight launches of Sparoair II vehicles had been conducted by 1961.[5] Each Sparoair II rocket cost US$6,000.[6]

Sparoair III

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Sparoair III utilised a redesigned second-stage motor, and could be launched from the F-4 Phantom II; however, any aircraft capable of launching the Sparrow III AAM could launch the Sparoair.[5]

The Sparoair III utilised the aircraft's Low Altitude Bombing System (LABS) circuits to initiate launch; the second stage was ignited via a mechanical device armed by the acceleration of the first stage.[5]

The first Sparoair III was launched on 8 July 1965; it proved a partial failure as the second stage failed to ignite. The second launch on 26 May 1966 failed after six seconds of second-stage burn when the vehicle exploded.[5] No further launches were undertaken.[4]

Version table

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The following table summarizes the different configurations:[4][1][2][3]

Version Aircraft Stage 1 Stage 2 First Launch Last Launch Number
Sparoair I F3H (F-3) Demon, F4D (F-6) Skyray Sparrow Sparrow 1960 1964-01-18 4
Sparoair II F3H (F-3) Demon, F4D (F-6) Skyray Sparrow Sparrow 1961 1961 >8
Sparoair III F-4 Phantom II Sparrow 22.6KS1245 1965-07-08 1966-05-26 2

References

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  4. ^ a b c Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  5. ^ a b c d e f Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).[dead ftp link] (To view documents see Help:FTP)
  6. ^ a b c Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  7. ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).
  8. ^ Lua error in Module:Citation/CS1/Configuration at line 2172: attempt to index field '?' (a nil value).