Juno I

Juno I

Juno I satellite launch vehicle. (USAF)
Function Orbital launch vehicle
Manufacturer Chrysler for the ABMA
Country of origin United States
Size
Height 21.2 m (70 ft)
Diameter 1.78 m (5 ft 10 in)
Mass 29,060 kg (64,070 lb)
Stages 4
Capacity
Payload to LEO 11 kg (24 lb)
Launch history
Status Retired
Launch sites LC-5 and 26A, Cape Canaveral Missile Annex, Florida
Total launches 6
Successes 3
Failures 3
First flight January 31, 1958
Last flight October 23, 1958
First stage - Redstone (stretched)
Engines 1x Rocketdyne A-7
Thrust 42,439 kgf (416.18 kN; 93,560 lbf)
Specific impulse 235 sec
Burn time 155 seconds
Fuel Hydyne/LOX
Second stage - MGM-29 Sergeant cluster
Engines 11 Solid
Thrust 7,480 kgf (73.4 kN; 16,500 lbf)
Specific impulse 214 sec
Burn time 6 seconds
Fuel Solid - polysulfide-aluminum and ammonium perchlorate
Third stage - MGM-29 Sergeant cluster
Engines 3 Solid
Thrust 2,040 kgf (20.0 kN; 4,500 lbf)
Specific impulse 214 sec
Burn time 6 seconds
Fuel Solid - polysulfide-aluminum and ammonium perchlorate
Fourth stage - MGM-29 Sergeant
Engines 1 Solid
Thrust 680 kgf (6.7 kN; 1,500 lbf)
Specific impulse 214 sec
Burn time 6 seconds
Fuel Solid - polysulfide-aluminum and ammonium perchlorate

The Juno I was a four-stage American booster rocket which launched America's first satellite, Explorer 1, in 1958. A member of the Redstone rocket family, it was derived from the Jupiter-C sounding rocket. It is commonly confused with the Juno II launch vehicle, which was derived from the PGM-19 Jupiter medium-range ballistic missile.

Development

The Juno I consisted of a Jupiter-C rocket, with a fourth stage mounted on top of the "tub" of the third stage, which was fired after third stage burnout to boost the payload and fourth stage to an orbital velocity of 8 kilometres per second (29,000 km/h; 18,000 mph). This multi-stage system, designed by Wernher von Braun in 1956 for his proposed Project Orbiter, obviated the need for a guidance system in the upper stages, proving to be the simplest and most immediate method for putting a payload into orbit; but as it had no upper-stage guidance, it could not inject the payload into a precise orbit. Both the four-stage Juno I and three-stage Jupiter-C launch vehicles were the same height (21.2 meters), with the added fourth-stage booster of the Juno I being enclosed inside the nose cone of the third stage.

The rocket family is named for the Roman goddess and queen of the gods Juno for its position as the satellite-launching version of the Jupiter-C. The name was proposed by JPL Director Dr. William Pickering in November 1957. The September 1956 test launch of a Jupiter-C for the Army Ballistic Missile Agency could have been the world's first satellite launch. Had the fourth stage been loaded and fueled, the nose cone would have overshot the target and entered orbit. Such a launch did not occur until early 1958 when a Juno 1 successfully launched the first United States satellite, Explorer 1, as part of Project Vanguard, after the Soviet Union's Sputnik 1 in October 1957.[1]

History

Although Juno I's launch of the Explorer 1 satellite was a huge success for the U.S. space program, only two of its remaining five flights were successful; launching Explorer 3 and 4. The American public was happy and relieved that America had finally managed to launch a satellite after the launch failures in the Vanguard and Viking series. With the relative success of the Juno I program, von Braun developed the Juno II, using a PGM-19 Jupiter first stage, rather than a Redstone.

The six launches of Juno I were:

Gallery

Juno I carrying Explorer 3
Juno I with Explorer I mock-up at Kennedy Space Center

References

  1. Bello, Francis (1959). "The Early Space Age". Fortune. Retrieved June 5, 2012.
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