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Able (rocket stage)

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(Redirected fromAblestar)
American rocket stage
Able rocket stage
Able rocket stage, is the second stage in the Vanguard rocket cutaway view
Able rocket stage engine in the foreground

TheAble rocket stage was arocket stage manufactured in the United States byAerojet as the second of three stages of theVanguard rocket used in theVanguard project from 1957 to 1959. The Able stage name represents its place as the first in the series, from theJoint Army/Navy Phonetic Alphabet.[1]

To save weight Aerojet used analuminum tube for the enginethrust chamber. Theengine used on Vanguard was anAJ10-37, burningnitric acid andUDMH asrocket propellants.On later Able models rockets the AJ10-41 and AJ10-42 engines were used. Aerojet made 21 Able rocket stages for use on launchers.[2] The Vanguard project launched 11 Able stages. Three putsatellites intoorbit:Vanguard 1,Vanguard 2 andVanguard 3. The Able rocket stage and the Vanguard project were an important part of theSpace Race between the US andSoviet Union.[citation needed] The AJ10 engines used in the Able rocket stage continue to be used on later rockets and are still in use. In honor of the rocket stage during ananimals in space test, arhesus monkey named Miss Able, flew withMiss Baker on May 28, 1959.[3] Later Able stages usedAJ10-101 or AJ10-101A rocket engines.

The Able rocket stage was discontinued in 1960. A version of the AJ10 engine used for the Able rocket stage was used as the engine ofApollo Service Module.[4]

The improved Able-Star version was used as the upper stage of theThor-Ablestar two stage launcher. The Able-Star second stage was an enlarged version of the Able rocket stage using AJ10-104 or AJ10-104D engines, which gave the Thor-Ablestar a greaterpayload capacity compared to the earlierThor-Able.[5] It also incorporated restart capabilities, allowing a multiple-burntrajectory to be flown, further increasing payload, or allowing the rocket to reach differentorbits. It was the first rocket to be developed with such a capability and development of the stage took a mere eight months.[6]

Specifications

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Able

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  • Loaded gross mass: 1,884 kg (4,154 lb)[2]
  • Empty (unfueled) mass 429 kg (946 lb)[2]
  • Thrust 34.69 kN (7,800 lbf)[2]
  • Specific impulse (vacuum) 270 seconds (2.6 km/s)[2]
  • Height: 5.67 m (18.6 ft)[2]
  • Diameter: 0.81 m (2 ft 8 in)[2]
  • Span: 0.84 m (2 ft 9 in)[2]
  • Burn time: 115 seconds[2]
  • Engine: AJ10-40,AJ10-101[2]

Able-Star

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  • Loaded gross mass: 4,497 kg (9,914 lb)[5]
  • Empty (unfueled) mass 599 kg (1,321 lb)[5]
  • Thrust 36.02 kN (8,100 lbf)[5]
  • Specific impulse (vacuum) 280 seconds (2.7 km/s)[5]
  • Height: 4.52 m (14.8 ft)[5]
  • Diameter: 1.40 m (4 ft 7 in)[5]
  • Burn time: 296 seconds[5]
  • Engine: AJ10-104, AJ10-104D[5]

See also

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References

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  1. ^Helen T. Wells; Susan H. Whiteley; Carrie E. Karegeannes.Origin of NASA Names. NASA Science and Technical Information Office. p. 5.
  2. ^abcdefghijWade."Able".Encyclopedia Astronautica. Archived fromthe original on 2016-08-27. Retrieved2025-06-14.
  3. ^Darling, David."Able".www.daviddarling.info. Retrieved2025-06-14.
  4. ^The First Space Race: Launching the World's First Satellites, By Matt Bille, Erika Lishock, page 163 and page 174
  5. ^abcdefghi"Able-Star".www.astronautix.com. Retrieved2025-07-27.
  6. ^Wade, Mark."Delta". Encyclopedia Astronautica. Archived fromthe original on 24 July 2008. Retrieved30 November 2008.
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