Nike (rocket stage)

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Early Booster Missile Nike I (three fin model). Early-NikeI.jpg
Early Booster Missile Nike I (three fin model).

The Nike stage or Nike booster , a solid fuel rocket motor, was created by Hercules Aerospace for the Nike Ajax (M5) Nike Hercules (M5E1) (and M88 late in Hercules career). [1] [2] It was developed for use as the first stage of the Nike Ajax and Nike Hercules missiles as part of Project Nike. [3]

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It was subsequently employed in a variety of missiles and multi-stage sounding rockets, becoming one of the most popular and reliable rocket stages, not only in the United States, but also in several other countries around the world. [4]

Sounding rockets based on Nike Booster

A Nike Orion rocket in flight Nike-orion.jpg
A Nike Orion rocket in flight
A Nike Tomahawk photographed at Wallops Flight Facility. Nike tomahawk.jpg
A Nike Tomahawk photographed at Wallops Flight Facility.

See also

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Project Nike was a U.S. Army project, proposed in May 1945 by Bell Laboratories, to develop a line-of-sight anti-aircraft missile system. The project delivered the United States' first operational anti-aircraft missile system, the Nike Ajax, in 1953. A great number of the technologies and rocket systems used for developing the Nike Ajax were re-used for a number of functions, many of which were given the "Nike" name . The missile's first-stage solid rocket booster became the basis for many types of rocket including the Nike Hercules missile and NASA's Nike Smoke rocket, used for upper-atmosphere research.

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Titan IIIB was the collective name for a number of derivatives of the Titan II ICBM and Titan III launch vehicle, modified by the addition of an Agena upper stage. It consisted of five separate rockets. The Titan-3B Agena-D was a basic Titan IIIA with an Agena D upper stage. The Titan 23B was a basic Titan II with an Agena upper stage, and the Titan 24B was the same concept, but using the slightly enlarged Titan IIIM rocket as the base. The Titan 33B was a Titan 23B with the Agena enclosed in an enlarged fairing, in order to allow larger payloads to be launched. The final member of the Titan IIIB family was the Titan 34B which was a Titan 24B with the larger fairing used on the Titan 33B.

<span class="mw-page-title-main">Orion (rocket)</span>

Orion is the designation of a small American sounding rocket. The Orion has a length of 5.60 meters, a diameter of 0.35 m, a launch weight of 400 kg, a launch thrust of 7 kN and a ceiling of 85 kilometers. The Orion, built by NASA Goddard Space Flight Center's Wallops Flight Facility, is also used as an upper stage of sounding rockets, usually paired with a Terrier missile as the first stage, although Nike, Taurus and VS-30 rockets are also used.

Astrobee is the designation of series of American sounding rockets with one to three stages.

Nike Iroquois is the designation of a two-stage American sounding rocket. The Nike Iroquois was launched 213 times between 1964 and 1978. The maximum flight height of the Nike Iroquois amounts to 290 km (950,000 ft), the takeoff thrust 48,800 lbf (217 kN), the takeoff weight 700 kg and the length 8.00 m.

Nike Hydac is the designation of an American sounding rocket with two stages, based upon the Nike Ajax booster. The Nike Hydac was launched 87 times from many missile sites. Such sites were White Sands Missile Range, Poker Flat Research Range, Kwajalein Missile Range, Cassino Site - Rio Grande Airport, Brazil, and from North Truro Air Force Station in Massachusetts during Operation Have Horn in 1969.

Nike Nike was the designation of a two to four stage American sounding rocket consisting of two Nike stages and optional upper stages. These include the Hercules M5E1, M6, and X-220 solid rocket engines, the NOTS 'HPAG' solid rocket engine, and the Thiokol T-40, T-55, and 1.5KS35000 solid rocket engines. Nike Nike had a payload capacity of 70kg to a 352 km altitude, and was used 19 times between 1956 and 1979.

<span class="mw-page-title-main">Nike-Asp</span>

Nike Asp was an American sounding rocket. The Nike Asp has a ceiling of 220 km, a takeoff thrust of 217 kN, a takeoff weight of 700 kg, a diameter of 0.42 m and a length of 7.90 m.

The Nike-Cajun was a two-stage sounding rocket built by combining a Nike base stage with a Cajun upper stage. The Nike-Cajun was known as a CAN for Cajun And Nike. The Cajun was developed from the Deacon rocket. It retained the external size, shape and configuration of the Deacon but had 36 percent greater impulse than the Deacon due to improved propellant. It was launched 714 times between 1956 and 1976 and was the most frequently used sounding rocket of the western world. The Nike Cajun had a launch weight of 698 kg (1538 lb), a payload of 23 kg (51 lb), a launch thrust of 246 kN (55,300 lbf) and a maximum altitude of 120 km (394,000 ft). It had a diameter of 42 cm and a length of 7.70 m. The maximum speed of the Nike-Cajun was 6,760 km/h.

<span class="mw-page-title-main">Arcas (rocket)</span>

Arcas was the designation of an American sounding rocket, developed by the Atlantic Research Corp., Alexandria, Va.

The Grumman G-118 was a design for an all-weather missile-armed interceptor aircraft for use on US Navy aircraft carriers. Originally conceived as an uprated F11F Tiger, it soon evolved into a larger and more powerful project. Although two prototypes were ordered in 1955, development was cancelled the same year in favor of the F4H Phantom II before any examples were built. Grumman's next carrier fighter would be the F-14 Tomcat, ordered in 1968.

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<span class="mw-page-title-main">VSB-30</span> Brazilian sounding rocket

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<span class="mw-page-title-main">Kawasaki P-2J</span> Japanese maritime patrol aircraft

The Kawasaki P-2J is a maritime patrol and ASW aircraft developed for the Japan Maritime Self-Defense Force. A twin turboprop-powered version of the radial-engined P-2 Neptune, the P-2J was developed as an alternative to buying the larger and more expensive P-3 Orion, which would eventually replace the P-2J in the 1980s.

<span class="mw-page-title-main">Terasca</span>

Terasca, or Terrier-ASROC-Cajun, was an American three-stage sounding rocket developed and launched by the United States Navy. Derived from a combination of the Terrier, ASROC and Cajun rockets, three launches were attempted during 1959, but only one was successful.

The Cajun was an American sounding rocket developed during the 1950s. It was extensively used for scientific experiments by NASA and the United States military between 1956 and 1976.

Nike Yardbird was an American sounding rocket with two stages, based upon the Nike Hercules M5E1 booster and a Thiokol TE-289 Yardbird upper stage. Yardbird was an improved Thiokol XM-19 motor. The Nike Yardbird was launched 2 times from Wallops Island on Sphere Test aeronomy missions both of which were classified as failures. Information available does not state the reason for the mission failures but Astronautix lists the apogee of both missions as 10 km (6 mi) which is well below the goal of 120 km (70 mi).

References

  1. "Nike M5 (and M5E1, M88) Scale Data". 28 January 2012. Archived from the original on 2020-09-18. Retrieved 2020-09-21.
  2. 1 2 Parsch, Andreas. "Miscellaneous Nike-Boosted Rockets". Directory of U.S. Military Rockets and Missiles. pp. Appendix 4. Archived from the original on 2016-03-04. Retrieved 2016-03-03.
  3. "Ed Thelen's Nike Missile Web Site". Archived from the original on 2013-04-11. Retrieved 2013-04-23.
  4. 1 2 Corliss 1972 p. 24
  5. Nike-Deacon at Encyclopedia Astronautica
  6. Corliss 1972 p. 82
  7. Nike Javelin at Encyclopedia Astronautica
  8. Encyclopedia Astronautica Nike Malamute Info
  9. "Nike Orion". www.astronautix.com. Archived from the original on December 28, 2016. Retrieved 2019-06-01.
  10. Article title
  11. Corliss 1972 p. 63-64
  12. Nike Tomahawk
  13. Nike Viper I
  14. Krebs, Gunter. "Nike With Upper Stage". Gunter's Space Page. Archived from the original on 2016-03-04. Retrieved 2016-03-03.

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