Nike Hydac
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Nike Hydac
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 ("Poker Flats"), Kwajalein Missile Range, Cassino Site - Rio Grande Airport, Brazil, and from North Truro Air Force Station in Massachusetts during Operation Have Horn in 1969.astronautix.com: ''Nike Hydac''
The directing agency for Nike Hydac was the , (AFCRL)

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Sounding Rocket
A sounding rocket or rocketsonde, sometimes called a research rocket or a suborbital rocket, is an instrument-carrying rocket designed to take measurements and perform scientific experiments during its sub-orbital flight. The rockets are used to launch instruments from 48 to 145 km (30 to 90 miles) above the surface of the Earth, the altitude generally between weather balloons and satellites; the maximum altitude for balloons is about 40 km (25 miles) and the minimum for satellites is approximately 121 km (75 miles). Certain sounding rockets have an apogee between 1,000 and 1,500 km (620 and 930 miles), such as the Black Brant X and XII, which is the maximum apogee of their class. Sounding rockets often use military surplus rocket motors. NASA routinely flies the Terrier Mk 70 boosted Improved Orion, lifting 270–450-kg (600–1,000-pound) payloads into the exoatmospheric region between 97 and 201 km (60 and 125 miles). Etymology The origin of the te ...
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Nike-Asp
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-Asp is an Asp rocket with a Nike booster system. It was at times ship-launched. After NASA took control of the project, the rocket fell into disuse. USS Point Defiance (LSD-31) USS Point Defiance (LSD-31) became one of the first rocket-launching surface ships to support the 1958 IGY Solar Eclipse Expedition to the Pukapuka, Danger Island region of the South Pacific. Launchers on deck fired eight Nike-Asp model LV sounding rockets to collect scientific data during the eclipse. Each USN solar XUV and X-ray detection launch (5 as a salvo) was from 40.0° N 150.0° W on Oct 12 1958 - at 08:32, 08:42, 08:43, 08:52, and 09:10 GMT, with configuration designations: NN8.59F - NN8.62F and successive apogee achievements of 222, 236, 242, 240, and 88 km. Vandenberg Air Force Base Bet ...
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Nike Tomahawk
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). It was developed for use as the first stage of the Nike Ajax and Nike Hercules missiles as part of Project Nike. 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.Corliss 1972 p. 24 Sounding rockets based on Nike Booster *The Nike Deacon has a ceiling of 189 km, a takeoff thrust of 217 kN, a takeoff weight of 710 kg, a diameter of 0.42 m and a length of 7.74 m. * The Nike Javelin was launched 34 times between 1964 and 1978. The maximum flight altitude of the Nike Javelin was 130 km, the takeoff thrust 217 kN, takeoff weight 900 kg, 0.42 m and length 8.20 m. * The Nike Malemute consists ...
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Nike T40 T55
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). It was developed for use as the first stage of the Nike Ajax and Nike Hercules missiles as part of Project Nike. 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.Corliss 1972 p. 24 Sounding rockets based on Nike Booster *The Nike Deacon has a ceiling of 189 km, a takeoff thrust of 217 kN, a takeoff weight of 710 kg, a diameter of 0.42 m and a length of 7.74 m. * The Nike Javelin was launched 34 times between 1964 and 1978. The maximum flight altitude of the Nike Javelin was 130 km, the takeoff thrust 217 kN, takeoff weight 900 kg, 0.42 m and length 8.20 m. * The Nike Malemute consists ...
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Nike Recruit
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). It was developed for use as the first stage of the Nike Ajax and Nike Hercules missiles as part of Project Nike. 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.Corliss 1972 p. 24 Sounding rockets based on Nike Booster *The Nike Deacon has a ceiling of 189 km, a takeoff thrust of 217 kN, a takeoff weight of 710 kg, a diameter of 0.42 m and a length of 7.74 m. * The Nike Javelin was launched 34 times between 1964 and 1978. The maximum flight altitude of the Nike Javelin was 130 km, the takeoff thrust 217 kN, takeoff weight 900 kg, 0.42 m and length 8.20 m. * The Nike Malemute consists of ...
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Nike Orion
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). It was developed for use as the first stage of the Nike Ajax and Nike Hercules missiles as part of Project Nike. 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.Corliss 1972 p. 24 Sounding rockets based on Nike Booster *The Nike Deacon has a ceiling of 189 km, a takeoff thrust of 217 kN, a takeoff weight of 710 kg, a diameter of 0.42 m and a length of 7.74 m. * The Nike Javelin was launched 34 times between 1964 and 1978. The maximum flight altitude of the Nike Javelin was 130 km, the takeoff thrust 217 kN, takeoff weight 900 kg, 0.42 m and length 8.20 m. * The Nike Malemute consists ...
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Nike-Nike
Nike Nike is the designation of a United States sounding rocket. The Nike Nike consists of two Nike Nike often refers to: * Nike (mythology), a Greek goddess who personifies victory * Nike, Inc., a major American producer of athletic shoes, apparel, and sports equipment Nike may also refer to: People * Nike (name), a surname and feminine give ... rocket booster stages (and if necessary a further rocket stage) and reaches a ceiling of 352 km. The Nike Nike was used 16 times between 1954 and 1979. References Nike (rocket family) {{rocket-stub ...
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Nike Malemute
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). It was developed for use as the first stage of the Nike Ajax and Nike Hercules missiles as part of Project Nike. 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.Corliss 1972 p. 24 Sounding rockets based on Nike Booster *The Nike Deacon has a ceiling of 189 km, a takeoff thrust of 217 kN, a takeoff weight of 710 kg, a diameter of 0.42 m and a length of 7.74 m. * The Nike Javelin was launched 34 times between 1964 and 1978. The maximum flight altitude of the Nike Javelin was 130 km, the takeoff thrust 217 kN, takeoff weight 900 kg, 0.42 m and length 8.20 m. * The Nike Malemute consists ...
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Nike Javelin
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). It was developed for use as the first stage of the Nike Ajax and Nike Hercules missiles as part of Project Nike. 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.Corliss 1972 p. 24 Sounding rockets based on Nike Booster *The Nike Deacon has a ceiling of 189 km, a takeoff thrust of 217 kN, a takeoff weight of 710 kg, a diameter of 0.42 m and a length of 7.74 m. * The Nike Javelin was launched 34 times between 1964 and 1978. The maximum flight altitude of the Nike Javelin was 130 km, the takeoff thrust 217 kN, takeoff weight 900 kg, 0.42 m and length 8.20 m. * The Nike Malemute consists of ...
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Nike-Iroquois
Nike Iroquois is the designation of a two-stage American sounding rocket A sounding rocket or rocketsonde, sometimes called a research rocket or a suborbital rocket, is an instrument-carrying rocket designed to take measurements and perform scientific experiments during its sub-orbital flight. The rockets are used to .... 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. References *Nike-Iroquoisat Encyclopedia Astronautica Nike (rocket family) {{rocket-stub ...
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Nike-Deacon
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). It was developed for use as the first stage of the Nike Ajax and Nike Hercules missiles as part of Project Nike. 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.Corliss 1972 p. 24 Sounding rockets based on Nike Booster *The Nike Deacon has a ceiling of 189 km, a takeoff thrust of 217 kN, a takeoff weight of 710 kg, a diameter of 0.42 m and a length of 7.74 m. * The Nike Javelin was launched 34 times between 1964 and 1978. The maximum flight altitude of the Nike Javelin was 130 km, the takeoff thrust 217 kN, takeoff weight 900 kg, 0.42 m and length 8.20 m. * The Nike Malemute consists of ...
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Nike-Cajun
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 (1 ft 4 in) and a length of 7.70 m (25 ft 3 in). The maximum speed of the Nike-Cajun was . The Cajun stage of this rocket was named for the Cajun people of south Louisiana because one of the rocket's designers, J. G. Thibodaux, was a Cajun. The Nike ...
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