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rocket

Did you mean: rocket (in aeronautics), Houston Rockets (Sports - NBA), rocket, rocket (in botany), rocket, rocket, rocket (sign language), rocket, Rockets (band), Rockets (album)

 
Dictionary: rock·et1

n.
    1. A rocket engine.
    2. A vehicle or device propelled by one or more rocket engines, especially such a vehicle designed to travel through space.
  1. A projectile weapon carrying a warhead that is powered and propelled by rockets.
  2. A projectile firework having a cylindrical shape and a fuse that is lit from the rear.

v., -et·ed, -et·ing, -ets.

v.intr.
  1. To move swiftly and powerfully, as a rocket
  2. To fly swiftly straight up, as a game bird frightened from cover.
  3. To soar or rise rapidly: The book rocketed to the top of the bestseller list.
v.tr.
  1. To carry by means of a rocket.
  2. To assault with rockets.

[Italian rocchetta, diminutive of rocca, spindle, distaff, of Germanic origin.]


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rocket
Type of jet-propulsion device that uses either solid or liquid propellants to provide the fuel and oxidizer needed for combustion. The hot gases provided by combustion are ejected in a jet through a nozzle at the rear of the rocket. The term is also commonly applied to any of various vehicles, including fireworks, skyrockets, guided missiles, and launch vehicles for spacecraft, that are driven by such a propulsive device. Typically, thrust (force causing forward motion) is produced by reaction to a rearward expulsion of hot gases at extremely high speed (see Newton's laws of motion).

For more information on rocket, visit Britannica.com.

Either a propulsion system or a complete vehicle driven by such a propulsive engine. A rocket engine provides the means whereby chemical matter is burned to release the energy stored in it and the energy is expended, by ejection at high velocity of the products of combustion (the working fluid). The ejection imparts motion to the vehicle in a direction opposite to that of the ejected matter. A rocket vehicle is propelled by rocket reaction and includes all components necessary for such propulsion, and a payload such as an explosive charge, scientific instruments, or a crew. A rocket vehicle also includes guidance and control equipment mounted in a structural air-frame or spaceframe. See also Rocket propulsion; Rocket staging; Satellite (spacecraft); Space flight; Space probe.


Thesaurus:

rocket

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verb

  1. To move swiftly: bolt, bucket, bustle, dart, dash, festinate, flash, fleet, flit, fly, haste, hasten, hurry, hustle, pelt2, race, run, rush, sail, scoot, scour2, shoot, speed, sprint, tear1, trot, whirl, whisk, whiz, wing, zip, zoom. Informal hotfoot, rip. Slang barrel, highball. Chiefly British nip1. Idioms: get a move on, get cracking, go like lightning, go like the wind, hotfoot it, make haste, make time, make tracks, run like the wind, shake a leg, stepjumpon it. See move/halt.
  2. To rise abruptly and precipitously: sky, skyrocket, soar. Informal shoot up. See increase/decrease.

In their most basic form, rockets are uncomplicated machines. They comprise a fuel supply, a combustion chamber in which the fuel is burnt, and a nozzle through which the products of combustion—mostly hot gasses—can escape. Early rockets were little more than tubes closed at one end and filled with gunpowder. They were used for fireworks and for maritime rescue (as signals and carriers of lifelines), but they lacked the power and accuracy to be useful beyond these highly specialized niches. Military interest in gunpowder rockets was sporadic and limited. The British use of them to bombard Fort McHenry, near Baltimore during the War of 1812, for example, did more for American culture (by inspiring Francis Scott Key to write "The Star Spangled Banner") than it did for British military objectives.

Modern rockets emerged between 1920 and 1960 from the confluence of several technological breakthroughs: more powerful fuels, lighter structural elements, steering mechanisms, onboard guidance systems, and multiple stages. These changes set the stage for the rocket's development, from the late 1950s on, into a range of powerful weapons and a versatile tool for scientific exploration.

The Birth of Modern Rocketry, 1920–1960

Robert H. Goddard was the spiritual father but not the true founder of American rocketry. He tested his first solid-fuel rocket on 7 November 1918 and the world's first liquid-fueled rocket (burning gasoline and liquid oxygen) on 16 March 1926. Trained as a physicist, Goddard produced rockets notable more for innovative design features than for sound engineering. He also feared that rivals might steal his ideas—an obsession that led him to publish few papers and keep potential collaborators at arm's length. His genius was prodigious, but his influence was slight.

The foundations of American rocketry were laid, in a practical sense, by four small groups of scientists and engineers scattered across the country. The first of these groups, the American Rocket Society, was formed as the American Interplanetary Society in 1930 by a group of technically minded New York City science fiction writers (they renamed their group in 1934). Its leading members went on to found Reaction Motors, one of America's first rocket-building companies. A second important group coalesced in the late 1930s around aerodynamics expert Theodore von Karman at the California Institute of Technology (Cal Tech). In time this group gave rise to another early rocket-building firm: Aerojet. A third group, led by naval officer Robert Truax, formed in the late 1930s at the Naval Research Laboratory in Annapolis, Maryland. The fourth group consisted of 115 scientists and engineers from Germany's wartime rocket program, led by the charismatic Wernher von Braun and hired by the U.S. Army to apply their expertise to its nascent rocket-building program. They brought with them boxes of technical documents and scores of V-2 rockets—then the world's most advanced—in various stages of assembly. Reassembling and test-firing the V-2s under the Germans' direction gave army rocket experts their first practical experience with large ballistic missiles.

All four groups worked closely with the military. Von Braun's and Truax's were directly supported by the army and navy, respectively. Von Karman worked closely with General Henry H. "Hap" Arnold, commander of the U. S. Army Air Forces. Reaction Motors supplied the engines for most of the Air Force's experimental rocket planes, including the Bell X-1 that broke the "sound barrier" in 1947. Through their military projects, the rocket designers also made connections with established defense contractors. The foundations of a robust aerospace industry had thus been laid even before the end of World War II.

The rockets that emerged from these collaborations in the late 1940s and early 1950s established the basic design elements used by American rockets for the rest of the century. These included multiple stages (1947), lightweight aluminum rocket bodies that doubled as fuel tanks (1948), and swiveling engines for steering (1949). High-energy kerosene derivatives replaced gasoline and alcohol in liquid-fuel rockets. Research at Cal Tech produced a viscous solid fuel that produced more power and higher reliability than traditional powders. Thiokol Chemical Corporation improved it and by the 1950s had enabled solid-fuel rockets to match the power of liquid-fuel ones. Combined, these features created a new generation of rockets. The first representatives—such as the Vanguard and Jupiter of the late 1950s—carried the first small American satellites into space. Later examples—such as Atlas and Titan of the early 1960s—had the power to carry a nuclear warhead halfway around the world or put a manned spacecraft into orbit.

Refinements and Applications, 1960–2000

President John F. Kennedy's May 1961 call to land a man on the moon "before this decade is out" gave von Braun and his team—then working for the National Aeronautics and Space Administration (NASA)—a chance to develop the largest rockets in history. The result was the Saturn V, which made possible nine lunar missions (six of them landings) between December 1968 and December 1972. Taller than the Statue of Liberty and heavier than a navy destroyer, the Saturn V generated the equivalent of 180 million horsepower at the moment of liftoff. However, the Saturn series was a technological dead end. No branch of the military had a practical use for so large a rocket, and (without the spur of a presidential challenge) the civilian space program could not afford to use them for routine exploration. Experiments with nuclear-powered rockets, pursued in the mid-1960s, were discontinued for similar reasons.

Saturn was, therefore, a typical of American rocket development after 1960. Specialization, rather than a continual push for more power and heavier payloads, was the dominant trend. The navy, for example, developed the Polaris—a solid-fuel missile capable of being carried safely aboard submarines and launched underwater. The air force developed the Minuteman as a supplement to the Atlas and Titan. It was smaller, but (because it used solid fuel) easier to maintain and robust enough to be fired directly from underground "silos." All three armed services also developed compact solid-fuel missiles light enough to be carried by vehicles or even individual soldiers. Heat-seeking and radar-guided missiles had, by the Vietnam War (1964–1975), replaced guns as the principal weapon for air-to-air combat. They also emerged, in the course of that war, as the antiaircraft weapons most feared by combat pilots. Warships, after nearly four centuries serving principally as gun platforms, were redesigned as missile platforms in the 1960s and 1970s. "Wire-guided" missiles, first used in combat in October 1966, gave infantry units and army helicopter crews a combination of mobility, accuracy, and striking power once available only to tanks.

The space shuttle, NASA's followup to the Project Apollo moon landings, defined another line of rocket development. Conceived as a vehicle for cheap, reliable access to space, it was powered by three liquid-fuel engines aboard the winged orbiter and two large solid-fuel boosters jettisoned after launch. Both were designed to be reusable. The orbiter's engines would, according to the design specifications, be usable up to fifty times with only limited refurbishing between flights. The boosters, parachuted into the Atlantic Ocean after launch, would be cleaned, refurbished, and refilled with solid fuel for later reuse. By the early 2000s the shuttle, since becoming operational in 1981, had achieved neither the high flight rates nor the low costs its designers envisioned. Its reusability was, nonetheless, a significant achievement in a field where, for centuries, all rockets had been designed as disposable, single-use machines.

Bibliography

Bromberg, Joan Lisa. NASA and the Space Industry. Baltimore: Johns Hopkins University Press, 1999. Surveys NASA's evolving partnership with aerospace companies.

Heppenheimer, T. A. Countdown: A History of Space Flight. New York: John Wiley, 1997. Places rocket development in its social, political, and military context.

Ley, Willy. Rockets, Missiles, and Men into Space. New York: Viking, 1968. Dated, but useful for its lucid explanations and insider's view of early rocketry.

MacDougall, Walter A. The Heavens and the Earth. New York: Basic Books, 1985. Definitive history of the interplay of Cold War politics, military missiles, and the U. S. space program.

Winter, Frank. Rockets into Space. Cambridge, Mass.: Harvard University Press, 1990. A compact, nontechnical history of rocket technology.

 
rocket, any vehicle propelled by ejection of the gases produced by combustion of self-contained propellants. Rockets are used in fireworks, as military weapons, and in scientific applications such as space exploration.

Rocket Propulsion

The force acting on a rocket, called its thrust, is equal to the mass ejected per second times the velocity of the expelled gases. This force can be understood in terms of Newton's third law of motion, which states that for every action there is an equal and opposite reaction. In the case of a rocket, the action is the backward-streaming flow of gas and the reaction is the forward motion of the rocket. Another way of understanding rocket propulsion is to realize that tremendous pressure is exerted on the walls of the combustion chamber except where the gas exits at the rear; the resulting unbalanced force on the front interior wall of the chamber pushes the rocket forward. A common misconception, before space exploration pointed up its obvious fallacy, holds that a rocket accelerates by pushing on the atmosphere behind it. Actually, a rocket operates more efficiently in outer space, since there is no atmospheric friction to impede its motion.

Rocket Design

The key elements in designing a rocket are the propulsion system, which includes the propellant and the exit nozzle, and determining the number of stages required to lift the intended payload. Rocket navigation is usually based on inertial guidance; internal gyroscopes are used to detect changes in the position and direction of the rocket.

Rocket Propellants

The most vital component of any rocket is the propellant, which accounts for 90% to 95% of the rocket's total weight. A propellant consists of two elements, a fuel and an oxidant; engines that are based on the action-reaction principle and that use air instead of carrying their own oxidant are properly called jets. Propellants in use today include both liquefied gases, which are more powerful, and solid explosives, which are more reliable; the space shuttle's main engines use liquid propellant, while its boosters are solid-fuel rockets. The chemical energy of the propellants is released in the form of heat in the combustion chamber.

A typical liquid engine uses hydrogen as fuel and oxygen as oxidant; a typical solid propellant is nitroglycerine. In the liquid engine, the fuel and oxidant are stored separately at extremely low temperatures; in the solid engine, the fuel and oxidant are intimately mixed and loaded directly into the combustion chamber. A solid engine requires an ignition system, as does a liquid engine if the propellants do not ignite spontaneously on contact.

The efficiency of a rocket engine is defined as the percentage of the propellant's chemical energy that is converted into kinetic energy of the vehicle. During the first few seconds after liftoff, a rocket is extremely inefficient, for at least two unavoidable reasons: High power consumption is required to overcome the inertia of the nearly motionless mass of the fully fueled rocket; and in the lower atmosphere, power is wasted overcoming air resistance. Once the rocket gains altitude, however, it becomes more efficient. as the trajectory, at first vertical, curves into a suborbital arc or into the desired orbit.

Although all known rockets currently in use derive their energy from chemical reactions, more exotic propulsion systems are being considered. In ion propulsion, a plasma (ionized gas consisting of a mixture of positively charged atoms and negatively charged electrons) would be created by an electric discharge and then expelled by an electric field. The engine could provide a low thrust efficiently for long periods; on a lengthy flight this would produce very high velocities, so that if there is ever a trip to the outer planets an ion drive might be used. Deep Space 1, a space probe launched in 1998 to test new technologies, was propelled intermittently by an ion engine. Even nuclear power has been considered for propulsion; in fact, a nuclear ramjet was developed in the early 1960s before it was realized that because the exhaust gases would be highly radioactive such a drive could never be used in earth's atmosphere.

Design of the Exit Nozzle

A critical element in all rockets is the design of the exit nozzle, which must be shaped to obtain maximum energy from the exhaust gases moving through it. The nozzle usually converges to a narrow throat, then diverges to create a form which shapes the hypersonic flow of exhaust gas most efficiently. The walls of the combustion chamber and nozzle must be cooled to protect them against the heat of the escaping gases, whose temperature may be as high as 3,000°C-above the melting point of any metal or alloy.

Staging of Rockets

Although early rockets had only one stage, it was early recognized that no single-stage rocket can reach orbital velocity (5 mi/8 km per sec) or the earth's escape velocity (7 mi/11 km per sec). Hence multistage rockets, such as the two-stage Atlas-Centaur or the three-stage Saturn V, became necessary for space exploration. In these systems, two or more rockets are assembled in tandem and ignited in turn; once the lower stage's fuel is exhausted, it detaches and falls back to earth. Soviet systems clustered several rockets together, operated simultaneously, to obtain a large initial thrust.

Development of Rockets

The invention of the rocket is generally ascribed to the Chinese, who as early as A.D. 1000 stuffed gunpowder into sections of bamboo tubing to make military weapons of considerable effectiveness. The 13th-century English monk Roger Bacon introduced to Europe an improved form of gunpowder, which enabled rockets to become incendiary projectiles with a relatively long range. Rockets subsequently became a common if unreliable weapon. Major progress in design resulted from the work of William Congreve, an English artillery expert, who built a 20-lb (9-kg) rocket capable of traveling up to 2 mi (3 km). In the late 19th cent., the Austrian physicist Ernst Mach gave serious theoretical consideration to supersonic speeds and predicted the shock wave that causes sonic boom.

The astronautical use of rockets was cogently argued in the beginning of the 20th cent. by the Russian Konstantin E. Tsiolkovsky, who is sometimes called the "father of astronautics." He pointed out that a rocket can operate in a vacuum and suggested that multistage liquid-fuel rockets could escape the earth's gravitation. The greatest name in American rocketry is Robert H. Goddard, whose pamphlet A Method for Reaching Extreme Altitudes anticipated nearly all modern developments. Goddard launched the first liquid-fuel rocket in 1926 and demonstrated that rockets could be used to carry scientific apparatus into the upper atmosphere. His work found its most receptive audience in Germany. During World War II, a German team under Wernher von Braun developed the V-2 rocket, which was the first long-range guided missile. The V-2 had a range greater than 200 mi (322 km) and reached velocities of 3,500 mi (5,600 km) per hr.

After the war, rocket research in the United States and the Soviet Union intensified, leading to the development first of intercontinental ballistic missiles and then of modern spacecraft. Important U.S. rockets have included the Redstone, Jupiter, Atlas, Titan, Agena, Centaur, and Saturn carriers. Saturn V, the largest rocket ever assembled, developed 7.5 million lb (3.4 million kg) of thrust. A three-stage rocket, it stood 300 ft (91 m) high exclusive of payload and with the Apollo delivered a payload of 44 tons to the moon. Rockets presently being used to launch manned and unmanned missions into space include the Brazilian VSV-30; the Chinese Long March 2C, 2E, and 2F; the European Space Agency's Ariane 5 series; the Indian PSLV (Polar Satellite Launch Vehicle); the Israeli Shavit 2; the Russian Soyuz and Proton K and M; the Japanese H-2A; the South Korean-Russian KSLV-1; the U.S. Athena 1 and 2, Taurus, Titan 2 and 4B, Delta 2, 3, and 4, Atlas 2 ,3, and 5, and STS or space shuttle; and the multinational, private Sea Launch Zenit-3SL, which uses a converted oil platform located some 1,400 mi (2,250 km) southeast of Hawaii.

See also space science.

Bibliography

See G. P. Sutton, Rocket Propulsion Elements: An Introduction to the Engineering of Rockets (6th ed. 1992); F. H. Winter, Rockets into Space (1993); D. Baker, Spaceflight and Rocketry: A Chronology (1996); M. Stoiko, Pioneers of Rocketry (1997); R. Snedden, Rockets and Space (1998).


Word Tutor:

rocket

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pronunciation

IN BRIEF: A jet engine containing its own propellant and driven by reaction propulsion.

pronunciation We watched the rocket shoot into the air until it was out of sight.

Translations:

rockets

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Rocket

Dansk (Danish)
1.
n. - raket, raketdrevet rumfartøj, raketdrevet missil, [sl.] skideballe
v. intr. - bevæge sig hurtigt opad, stige voldsomt, ryge i vejret
v. tr. - bombardere med raketter

idioms:

  • rocket launcher    raketaffyringsrampe
  • rocket ship    raketdrevet rumfartøj

2.
n. - [bot.] salatsennep

Nederlands (Dutch)
raket, vuurpijl

Français (French)
1.
n. - fusée, (Mil) fusée
v. intr. - monter en flèche (des prix), passer en trombe
v. tr. - attaquer de rockets, porter au moyen d'une fusée

idioms:

  • rocket launcher    lanceur de fusée
  • rocket ship    vaisseau spatial

2.
n. - (Bot, Culin) roquette

Deutsch (German)
1.
n. - Rakete
v. - mit Raketen beschießen, in die Höhe schnellen

idioms:

  • rocket launcher    Raketenwerfer
  • rocket ship    Raketenschiff

2.
n. - Rauke, Barbarakraut

Ελληνική (Greek)
n. - πύραυλος, ρουκέτα, βολίδα, φωτοβολίδα, (φυτολ.) εσπερίς, ρόκα, (Βρετ., καθομ.) έντονη επίπληξη (κν. κατσάδα)
v. - εκτοξεύω/-ομαι, (μτφ.) ανέρχομαι στα ύψη, αυξάνομαι απότομα

idioms:

  • rocket launcher    (στρατ.) εκτοξευτής ρουκετών
  • rocket ship    διαστημόπλοιο, πυραυλάκατος

Italiano (Italian)
razzo, missile, fuoco d'artificio

idioms:

  • rocket launcher    lanciamissili
  • rocket ship    nave lanciamissili

Português (Portuguese)
n. - foguete (m), rojão (m)
v. - subir como um foguete

idioms:

  • rocket launcher    dispositivo lança-foguete
  • rocket ship    foguete (m)

Русский (Russian)
ракета, выговор, резко подниматься

idioms:

  • rocket launcher    пусковая ракетная установка
  • rocket ship    ракетоносец, ракетное судно

Español (Spanish)
1.
n. - cohete, misil, petardo
v. intr. - subir o elevarse como un cohete
v. tr. - bombardear o atacar con cohetes

idioms:

  • rocket launcher    lanzacohetes, lanzamisiles
  • rocket ship    nave espacial

2.
n. - juliana

Svenska (Swedish)
n. - raket, raketmotor, avhyvling
v. - skjuta iväg, skjuta i höjden, anfalla med raketvapen

中文(简体)(Chinese (Simplified))
1. 飞弹, 火箭, 火箭式投射器, 火箭发动机, 火箭弹, 向前急冲, 迅速上升, 飞快行进, 猛涨, 用火箭运载, 用火箭轰击

idioms:

  • rocket launcher    火箭发射装置, 火箭发射器, 火箭筒
  • rocket ship    火箭宇宙飞船, 火箭飞行器

2. 飞弹, 火箭, 火箭式投射器, 火箭发动机, 火箭弹

中文(繁體)(Chinese (Traditional))
1.
n. - 飛彈, 火箭, 火箭式投射器, 火箭發動機, 火箭彈
v. intr. - 向前急衝, 迅速上升, 飛快行進, 猛漲
v. tr. - 用火箭運載, 用火箭轟擊

idioms:

  • rocket launcher    火箭發射裝置, 火箭發射器, 火箭筒
  • rocket ship    火箭宇宙飛船, 火箭飛行器

2.
n. - 飛彈, 火箭, 火箭式投射器, 火箭發動機, 火箭彈

한국어 (Korean)
1.
n. - 로켓, 화전
v. intr. - 일직선으로 날아 오르다, 돌진하다
v. tr. - ~에 로켓을 발사하다, 로켓으로 쏘아 올리다

2.
n. - 평지과의 식물, 나도냉이

日本語 (Japanese)
n. - ロケット, ロケット弾, 打ち上げ花火, 狼煙, 厳しくしかること, 激しい叱責
v. - 急騰する, ロケットで打ち上げる, 突進する

idioms:

  • rocket launcher    ロケット弾発射機
  • rocket ship    ロケット船, 宇宙航空機

العربيه (Arabic)
‏(الاسم) صاروخ (فعل) يرتفع كالصاروخ‏

עברית (Hebrew)
n. - ‮טיל, רקטה, זיקוקית‬
v. intr. - ‮עלה במהירות, נעה אל על, נעה (חללית או רקטה)‬
v. tr. - ‮נעה/הסיעה (חללית או רקטה), נזף‬
n. - ‮אורה (צמח בר), גרגיר, בן חרדל מצוי (צמח בר)‬


 
 

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