Juno I

Last updated

  1. 1 2 Boehm, J.; Fichtner, H.J.; Hoberg, Otto A. Explorer satellites launched by Juno 1 and Juno 2 vehicles (PDF) (Report). US: NASA.PD-icon.svg This article incorporates text from this source, which is in the public domain .
  2. 1 2 3 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.
  4. 1 2 3 4 5 "Juno-1". Gunter's Space Page. Retrieved October 15, 2023.
  5. 1 2 "Juno-1 (5 stage)". Gunter's Space Page. Retrieved October 15, 2023.
Juno I
Juno I awaiting launch with Explorer I.jpg
Juno I awaiting launch with Explorer I
FunctionOrbital launch vehicle
Manufacturer Chrysler for the ABMA
Country of originUnited States
Size
Height21.2 m (70 ft)
Diameter1.78 m (5 ft 10 in)
Mass29,060 kg (64,070 lb)
Stages4
Capacity
Payload to LEO
Mass11 kg (24 lb)
Launch history
StatusRetired
Launch sites LC-5 and 26A,
Cape Canaveral Missile Annex, Florida
Total launches6
Success(es)3
Failure(s)3
First flight1 February 1958,
03:47:56 GMT
Last flightOctober 23, 1959
First stage – Redstone (stretched)
Powered by1 Rocketdyne A-7
Maximum thrust42,439 kgf (416.18 kN; 93,560 lbf)
Specific impulse 235 s (2.30 km/s)
Burn time155 seconds
Propellant Hydyne/LOX