Juno I

Juno I
	Juno I awaiting launch with Explorer I
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
Mass	11 kg (24 lb)
Launch history
Status	Retired
Launch sites	LC-5 and 26A,; Cape Canaveral Missile Annex, Florida
Total launches	6
Success(es)	3
Failure(s)	3
First flight	1 February 1958,; 03:47:56 GMT
Last flight	October 23, 1959
First stage – Redstone (stretched)
Powered by	1 Rocketdyne A-7
Maximum thrust	42,439 kgf (416.18 kN; 93,560 lbf)
Specific impulse	235 s (2.30 km/s)
Burn time	155 seconds
Propellant	Hydyne/LOX
Second stage – Baby Sergeant cluster
Powered by	11 Solid
Maximum thrust	7,480 kgf (73.4 kN; 16,500 lbf)
Specific impulse	220 s (2.2 km/s)
Burn time	6 seconds
Propellant	Polysulfide-aluminum and ammonium perchlorate (Solid)
Third stage – Baby Sergeant cluster
Powered by	3 Solid
Maximum thrust	2,040 kgf (20.0 kN; 4,500 lbf)
Specific impulse	236 s (2.31 km/s)
Burn time	6 seconds
Propellant	Polysulfide-aluminum and ammonium perchlorate (Solid)
Fourth stage – Baby Sergeant
Powered by	1 Solid
Maximum thrust	680 kgf (6.7 kN; 1,500 lbf)
Specific impulse	249 s (2.44 km/s)
Burn time	6 seconds
Propellant	Polysulfide-aluminum and ammonium perchlorate (Solid)
	[edit on Wikidata]

The Juno I was a four-stage American space launch vehicle, used to launch lightweight payloads into low Earth orbit. The launch vehicle was used between January 1958 to December 1959. 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 was derived from the PGM-19 Jupiter medium-range ballistic missile. In 1958, a Juno I launch vehicle was used to launch America's first satellite, Explorer 1.

History

Developed as a part of the Explorer Project, the original goal for the launch vehicle was to place an artificial satellite into orbit. Following the Soviet Union's launch of Sputnik 1 on October 4, 1957 (and the resulting "Sputnik crisis") and the failure of the Vanguard 1 launch attempt, the program received funding to match the Soviet space achievements. The launch vehicle family name was suggested in November 1957 by Jet Propulsion Laboratory (JPL) Director Dr. William Pickering, who proposed the name Juno, after the Roman goddess and queen of the gods, as well as for its position as the satellite-launching version of the Jupiter-C. The fourth stage for the Juno I launch vehicle was derived following the September 1956 test launch of a Jupiter-C for the Army Ballistic Missile Agency, which could have been the world's first satellite launch, had a fourth stage been loaded and fueled. A fourth stage would have allowed the nose cone to overshoot the target and enter orbit.^[2]

The first launch of a Juno I launch vehicle was in early 1958, with the successful launch of Explorer 1 satellite on February 1, 1958, at 03:47:56 GMT, after the Soviet Union's Sputnik 1 on October 4, 1957.^[2] The launch had been scheduled for January 29, 1958, but was scrubbed twice. Explorer 1 was the first U.S. satellite, and it confirmed the existence of the Van Allen radiation belt. Following the first successful launch, five more Juno I launch attempts occurred with two successes and three failures. The final launch attempt was on October 23, 1958, from Cape Canaveral Launch Pad 5, which ended in failure.^[3]

Launch vehicle

Juno I diagram

The Juno I consisted of a Jupiter-C first stage, based on the Redstone missile; with three additional solid fuel stages based on the Sergeant missile to provide the added impulse to achieve orbit.^[4] The fourth stage was mounted on top of the "tub" of the third stage, and fired after third-stage burnout to boost the payload and fourth stage to an orbital velocity of 8 km/s (5.0 mi/s), with an acceleration of 25–51 g. The tub along with the fourth stage were set spinning while the launch vehicle was on the launch pad to provide gyroscopic force in lieu of a guidance system that would have required thrust vectoring, vernier thrusters, or a reaction control system. The booster guidance package (with the tub attached) separated from the first stage after burnout to provide attitude control until second stage ignition.^[2] 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. It was the simplest method for putting a payload into orbit but having no upper-stage guidance, the payload could not achieve a precise orbit. Both the four-stage Juno I and three-stage Jupiter-C launch vehicles were the same height (21.2 m (70 ft)), with the added fourth-stage booster of the Juno I being enclosed inside the nose cone of the third stage.

Launch history

Juno I was launched six times by ABMA in 1958, intending to place satellites in LEO.^[4]^[5]

Following the successful launch of Explorer 1 on February 1, 1958, the first U.S. satellite, Juno I made five more launches before being retired in favor of Juno II.^[4] 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, Explorer 3 and Explorer 4,^[1] giving the Juno I vehicle a mission total success ratio of 50%.^[4] The Juno I vehicle was replaced by the Juno II in 1959.

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.

Juno I launches^[4]^[5]
Flight No.	Date / time (GMT)	Rocket	Launch site	Payload	Payload mass	Outcome	Comments
1	February 1, 1958 03:47:56	Juno I RS-29 (UE)	LC-26A	Explorer 1	22 kg	Success	Maiden launch of Juno I. First American satellite launched. Explorer 1 ceased transmission of data on May 23, 1958, when its batteries died, but remained in orbit for more than 12 years. It made a fiery reentry over the Pacific Ocean on March 31, 1970.
2	March 5, 1958 18:27:57	Juno I RS-26 (UV)	LC-26A	Explorer 2	23 kg	Failure	Fourth stage did not ignite.
3	March 26, 1958 17:38:03	Juno I RS-24 (UT)	LC-5	Explorer 3	23 kg	Success	Decay from orbit on June 28, 1958.
4	July 26, 1958 15:00:57	Juno I RS-44 (TT)	LC-5	Explorer 4	29 kg	Success	Decay from orbit on October 23, 1959.
5	August 24, 1958 06:17:22	Juno I RS-47 (TI)	LC-5	Explorer 5	29 kg	Failure	Booster collided with second stage after separation, causing upper stage firing angle to be off.
6	October 23, 1958 03:21:04	Juno I, RS-49 (HE)	LC-5	Beacon 1	23 kg	Failure	Five stage version, Second stage separated prematurely from booster.

Gallery

Juno I RS-29 UE launching Explorer 1
Juno I RS-26 UV launching Explorer 2
Juno I RS-24 UT launching Explorer 3
Juno I RS-44 TT with Explorer 4
Juno I RS-44 TT launching Explorer 4
Juno I RS-49 HE with BEACON 1
Juno I RS-49 HE launching BEACON 1
Juno I with Explorer 1 mock-up at the Kennedy Space Center rocket garden
Juno I with Explorer 1 mock-up at the National Air and Space Museum

References

^ ^a ^b Boehm, J.; Fichtner, H.J.; Hoberg, Otto A. Explorer satellites launched by Juno 1 and Juno 2 vehicles (PDF) (Report). US: NASA. This article incorporates text from this source, which is in the public domain.
^ ^a ^b ^c Bello, Francis (1959). "The Early Space Age". Fortune. Archived from the original on November 3, 2013. Retrieved June 5, 2012.
^ "JUNO I FACT SHEET". Spaceline. Retrieved August 1, 2021.
^ ^a ^b ^c ^d ^e "Juno-1". Gunter's Space Page. Retrieved October 15, 2023.
^ ^a ^b "Juno-1 (5 stage)". Gunter's Space Page. Retrieved October 15, 2023.

External links

Source: Data Sheet, Department of Astronautics, National Air and Space Museum, Smithsonian Institution.

[Boehm-NASA-1] Boehm, J.; Fichtner, H.J.; Hoberg, Otto A. Explorer satellites launched by Juno 1 and Juno 2 vehicles (PDF) (Report). US: NASA. This article incorporates text from this source, which is in the public domain.

[bello1959-2] Bello, Francis (1959). "The Early Space Age". Fortune. Archived from the original on November 3, 2013. Retrieved June 5, 2012.

[3] "JUNO I FACT SHEET". Spaceline. Retrieved August 1, 2021.

[:0-4] "Juno-1". Gunter's Space Page. Retrieved October 15, 2023.

[:1-5] "Juno-1 (5 stage)". Gunter's Space Page. Retrieved October 15, 2023.

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v t e Orbital launch systems
List of orbital launch systems Comparison of orbital launch systems
Current	Angara 1.2 A5 Ariane 6 Atlas V Ceres 1 1S Chollima-1 Electron Falcon 9 Block 5 Falcon Heavy Firefly Alpha Gravity-1 GSLV H-IIA H3 Hyperbola-1 Jielong 1 3 KAIROS^† Kaituozhe 2 Kinetica 1 Kuaizhou 1 1A 11 Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 6A 7 7A 8 11 11H LVM3 Minotaur I IV V C Nuri OS-M1^† Pegasus XL Proton-M PSLV Qaem 100 Qased Shavit 2 Simorgh SLS Block 1 Soyuz-2 2.1a / STA 2.1b / STB 2-1v SSLV Starship Tianlong-2 Unha Vega C Vulcan Centaur Zhuque 2
In development	Antares 330 Bloostar Cyclone-4M Deca Epsilon S Eris Gravity-2 Hyperbola-2 Irtysh Kuaizhou 21 31 Long March 9 10 12 Miura 5 MLV Neutron New Glenn New Line 1 NGLV Nova OS-M 2 4 Orbex Prime Pallas-1 Red Dwarf SLS Block 1B Block 2 Soyuz-7 Terran R Tianlong-3 VLM Vega E Zero Zhuque 3 Zuljanah
Retired	Antares 110 120 130^† 230 230+ Ariane 1 2 3 4 5 ASLV Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able^† Agena Centaur Black Arrow Conestoga^† Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV IV Heavy Diamant Dnepr Energia Epsilon Europa I^† II^† Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" Feng Bao 1 GSLV Mk I H-I H-II H-IIB Juno I Juno II Kaituozhe-1 Kosmos original 1 2/2I 3 3M Lambda 4S LauncherOne Long March 1 1D^† 2A 2E 3 3B 4A Mu 4S 3C 3H 3S 3SII V N1^† N-I N-II Naro-1 Paektusan^† Pilot-2^† R-7 Luna Molniya M L Polyot Soyuz original FG L M U U2 Soyuz/Vostok Sputnik Voskhod Vostok L K 2 2M R-29 Shtil' Volna^† Rocket 3 RS1^† Safir 1 1A 1B Saturn I IB V Scout X-1 Blue Scout II^† X-2^† X-2M X-3 X-3M X-4 X-2B^† B A B-1 D-1 A-1 E-1 F-1 G-1 Shavit original 1 SLV Space Shuttle SPARK^† Sparta SS-520 Start-1 Terran 1^† Thor Able Ablestar 1 2 Agena A B D Burner 1 2 Delta DSV-2U Thorad-Agena SLV-2G SLV-2H Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Tsyklon R-36-O original 2 3 Universal Rocket UR-500 Proton Proton-K Rokot Strela Vanguard Vega original VLS-1^† Zenit 2 2M 2FG 3SL 3SLB 3F Zhuque 1^†
Classes	Sounding rocket Small-lift launch vehicle Medium-lift launch vehicle Heavy-lift launch vehicle Super heavy-lift launch vehicle
This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future Symbol ^† indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)

v t e Orbital launch systems developed in the United States
Active	Atlas V**^†† Electron Falcon 9 Block 5 Falcon Heavy Firefly Alpha Minotaur I IV V C Pegasus XL SLS Block 1 Vulcan Centaur
In development	Antares 330 Daytona I MLV New Glenn Neutron Nova Red Dwarf SLS Block 1B Block 2 Starship Terran R
Retired	Antares 110/120/130/230/230+^††† Athena I II Atlas B D E/F G H I II III LV-3B SLV-3 Able Agena Centaur Conestoga Delta A B C D E G J L M N 0100 1000 2000 3000 4000 5000 II III IV IV Heavy Falcon 1 Falcon 9 v1.0 v1.1 v1.2 "Full Thrust" H-I* Juno I Juno II LauncherOne N-I* N-II* Pilot Rocket 3 RS1^† Saturn I IB V Scout Space Shuttle SPARK Sparta Terran 1 Thor Able Ablestar Agena Burner Delta DSV-2U Thorad-Agena Titan II GLV IIIA IIIB IIIC IIID IIIE 34D 23G CT-3 IV Vanguard
* - Japanese projects using US rockets or stages ** - uses Russian engines ^† - never succeeded ^†† - no new orders accepted ^††† - used Ukrainian first stage