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Juno I

The Juno I is a series of a four-stage American space launch vehicle that was used to launch lightweight payloads into low Earth orbit from January 1958 to October 1958. The launch vehicle is a member of the Redstone launch vehicle family, and was derived from the Jupiter-C sounding rocket. It is commonly confused with the Juno II launch vehicle, which…

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Burn time
155 seconds · 6 seconds
Country of origin
United States
Diameter
1.78 m (5 ft 10 in)
Failure
3
First flight
1 February 1958, 03:47:56 GMT
Function
Orbital launch vehicle

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Overview

History

Launch vehicle

Launch history

On display

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Juno I

Nodes46
Edges45
Triples90
Avg. degree1.96
Density0.043478
Components1

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Juno I

Top relations

related to history · 31
Juno I → ABMA, Although Juno I's, Army Ballistic Missile Agency, Cape Canaveral Launch Pad, Developed, Director Dr, Earth, Explorer, Explorer Project, February, Following, GMT, January, Jet Propulsion Laboratory, JPL, Juno, Juno II, Jupiter-C, November, October
related to Launch vehicle · 12
Juno I → Both, Braun, It, Juno, Jupiter-C, Project Orbiter, Redstone, Sergeant, The, The Juno, This, Wernher
related to Gallery · 8
Juno I → BEACON, Explorer, Juno, RS-24 UT, RS-26 UV, RS-29 UE, RS-44 TT, RS-49 HE
related to On display · 6
Juno I → Air, Explorer, Juno, Jupiter-C, Kennedy Space Center, Space Museum
Maximum thrust · 4
Juno I → 2,040 kgf (20.0 kN; 4,500 lbf), 42,439 kgf (416.18 kN; 93,560 lbf), 680 kgf (6.7 kN; 1,500 lbf), 7,480 kgf (73.4 kN; 16,500 lbf)
Powered by · 4
Juno I → 1 Rocketdyne A-7, 1 Solid, 11 Solid, 3 Solid
Specific impulse · 4
Juno I → 220 s (2.2 km/s), 235 s (2.30 km/s), 236 s (2.31 km/s), 249 s (2.44 km/s)
Burn time · 2
Juno I → 155 seconds, 6 seconds
Mass · 2
Juno I → 11 kg (24 lb), 29,060 kg (64,070 lb)
Propellant · 2
Juno I → Hydyne/LOX, Polysulfide-aluminum and ammonium perchlorate (Solid)

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Important terminology

juno launch vehicle first explorer jupiter-c satellite 1958 orbit stage missile ii successful space october used derived success following fourth

Entity relationships Subject–Predicate–Object triples

SubjectPredicateObjectConfidenceSrc
Juno IBurn time155 seconds1.00infobox
Juno IBurn time6 seconds1.00infobox
Juno ICountry of originUnited States1.00infobox
Juno IDiameter1.78 m (5 ft 10 in)1.00infobox
Juno IFailure31.00infobox
Juno IFirst flight1 February 1958, 03:47:56 GMT1.00infobox
Juno IFunctionOrbital launch vehicle1.00infobox
Juno IHeight21.2 m (70 ft)1.00infobox
Juno ILast flightOctober 23, 19591.00infobox
Juno ILaunch sitesLC-5 and 26A, Cape Canaveral Missile Annex, Florida1.00infobox
Juno IManufacturerChrysler for the ABMA1.00infobox
Juno IMass29,060 kg (64,070 lb)1.00infobox
Juno IMass11 kg (24 lb)1.00infobox
Juno IMaximum thrust42,439 kgf (416.18 kN; 93,560 lbf)1.00infobox
Juno IMaximum thrust7,480 kgf (73.4 kN; 16,500 lbf)1.00infobox
Juno IMaximum thrust2,040 kgf (20.0 kN; 4,500 lbf)1.00infobox
Juno IMaximum thrust680 kgf (6.7 kN; 1,500 lbf)1.00infobox
Juno IPowered by1 Rocketdyne A-71.00infobox
Juno IPowered by11 Solid1.00infobox
Juno IPowered by3 Solid1.00infobox
Juno IPowered by1 Solid1.00infobox
Juno IPropellantHydyne/LOX1.00infobox
Juno IPropellantPolysulfide-aluminum and ammonium perchlorate (Solid)1.00infobox
Juno ISpecific impulse235 s (2.30 km/s)1.00infobox
Juno ISpecific impulse220 s (2.2 km/s)1.00infobox
Juno ISpecific impulse236 s (2.31 km/s)1.00infobox
Juno ISpecific impulse249 s (2.44 km/s)1.00infobox
Juno IStages41.00infobox
Juno IStatusRetired1.00infobox
Juno ISuccess(es)31.00infobox

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