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94-572: The missile was a three-stage, solid-fuelled system, capable of carrying up to eight W76 warheads in the Mark 4 RB. The first eight Ohio -class submarines were armed with Trident I missiles. Twelve James Madison - and Benjamin Franklin -class submarines were also retrofitted with Trident I missiles, which replaced older Poseidon missiles. In 1980, the Royal Navy requested Trident I missiles under

188-456: A 4.8 kg (11 lb) lead ball. The great general and divine cannons were the last indigenous Chinese cannon designs prior to the incorporation of European models in the 16th century. When the Portuguese reached China in the early 16th century, they were unimpressed with Chinese firearms compared with their own. With the progression of the earliest European arquebus to the matchlock and

282-412: A bore-filling projectile; rather, they were designed for the low-nitrate flamethrower fire lance that shot small coviative missiles. This was called the "bandit-striking penetrating gun" (ji zei bian chong). Some of these low–nitrate gunpowder flamethrowers used poisonous mixtures such as arsenious oxide , and would blast a spray of porcelain shards as fragmentation . Another fire lance described in

376-413: A casing, nozzle , grain ( propellant charge ), and igniter . The solid grain mass burns in a predictable fashion to produce exhaust gases, the flow of which is described by Taylor–Culick flow . The nozzle dimensions are calculated to maintain a design chamber pressure, while producing thrust from the exhaust gases. Once ignited, a simple solid rocket motor cannot be shut off, as it contains all

470-482: A control moment. For example, the Titan III C solid boosters injected nitrogen tetroxide for LITV; the tanks can be seen on the sides of the rocket between the main center stage and the boosters. An early Minuteman first stage used a single motor with four gimballed nozzles to provide pitch, yaw, and roll control. A typical, well-designed ammonium perchlorate composite propellant (APCP) first-stage motor may have

564-402: A frame shaped like a dragon, or else conveniently a tube of wood or bamboo to contain it. In the late 14th century, the rocket launching tube was combined with the fire lance. This involved three tubes attached to the same staff. As the first rocket tube was fired, a charge was ignited in the leading tube which expelled a blinding lachrymatory powder at the enemy, and finally the second rocket

658-541: A high-energy (yet unstable) monopropellant and the other acts as a lower-energy stabilizing (and gelling) monopropellant. In typical circumstances, nitroglycerin is dissolved in a nitrocellulose gel and solidified with additives. DB propellants are implemented in applications where minimal smoke is required yet a medium-high I sp of roughly 235 s (2.30 km/s) is required. The addition of metal fuels (such as aluminium ) can increase performance to around 250 s (2.5 km/s), though metal oxide nucleation in

752-564: A long history as the final boost stage for satellites due to their simplicity, reliability, compactness and reasonably high mass fraction . A spin-stabilized solid rocket motor is sometimes added when extra velocity is required, such as for a mission to a comet or the outer solar system, because a spinner does not require a guidance system (on the newly added stage). Thiokol's extensive family of mostly titanium-cased Star space motors has been widely used, especially on Delta launch vehicles and as spin-stabilized upper stages to launch satellites from

846-499: A loss in motor performance. Polyurethane-bound aluminium-APCP solid fuel was used in the submarine-launched Polaris missiles . APCP used in the space shuttle Solid Rocket Boosters consisted of ammonium perchlorate (oxidizer, 69.6% by weight), aluminium (fuel, 16%), iron oxide (a catalyst, 0.4%), polybutadiene acrylonitrile (PBAN) polymer (a non-urethane rubber binder that held the mixture together and acted as secondary fuel, 12.04%), and an epoxy curing agent (1.96%). It developed

940-594: A propellant mass fraction of 92.23% while the 14,000-kilogram (31,000 lb) Castor 30 upper stage developed for Orbital Science's Taurus II COTS (Commercial Off The Shelf) (International Space Station resupply) launch vehicle has a 91.3% propellant fraction with 2.9% graphite epoxy motor casing, 2.4% nozzle, igniter and thrust vector actuator, and 3.4% non-motor hardware including such things as payload mount, interstage adapter, cable raceway, instrumentation, etc. Castor 120 and Castor 30 are 2.36 and 2.34 meters (93 and 92 in) in diameter, respectively, and serve as stages on

1034-876: A range of 5,500 metres (3.4 mi). By the end of World War II total production of rocket launchers reached about 10,000. with 12 million rockets of the RS type produced for the Soviet armed forces. In the United States modern castable composite solid rocket motors were invented by the American aerospace engineer Jack Parsons at Caltech in 1942 when he replaced double base propellant with roofing asphalt and potassium perchlorate . This made possible slow-burning rocket motors of adequate size and with sufficient shelf-life for jet-assisted take off applications. Charles Bartley , employed at JPL (Caltech), substituted curable synthetic rubber for

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1128-487: A simple, solid-propellant rocket tube that was filled with gunpowder. One open end allowed the gas to escape and was attached to a long stick that acted as a guidance system for flight direction control. The first rockets with tubes of cast iron were used by the Kingdom of Mysore under Hyder Ali and Tipu Sultan in the 1750s. These rockets had a reach of targets up to a mile and a half away. These were extremely effective in

1222-414: A single-piece nozzle or 304 s (2.98 km/s) with a high-area-ratio telescoping nozzle. Aluminium is used as fuel because it has a reasonable specific energy density, a high volumetric energy density, and is difficult to ignite accidentally. Composite propellants are cast, and retain their shape after the rubber binder, such as Hydroxyl-terminated polybutadiene (HTPB), cross-links (solidifies) with

1316-943: A small charge that is set off when the propellant is exhausted after a time delay. This charge can be used to trigger a camera , or deploy a parachute . Without this charge and delay, the motor may ignite a second stage (black powder only). In mid- and high-power rocketry , commercially made APCP motors are widely used. They can be designed as either single-use or reloadables. These motors are available in impulse ranges from "A" (1.26 Ns– 2.50 Ns) to "O" (20.48 kNs – 40.96 kNs), from several manufacturers. They are manufactured in standardized diameters and varying lengths depending on required impulse. Standard motor diameters are 13, 18, 24, 29, 38, 54, 75, 98, and 150 millimeters. Different propellant formulations are available to produce different thrust profiles, as well as special effects such as colored flames, smoke trails, or large quantities of sparks (produced by adding titanium sponge to

1410-406: A specific impulse of 242 seconds (2.37 km/s) at sea level or 268 seconds (2.63 km/s) in a vacuum. The 2005-2009 Constellation Program was to use a similar PBAN-bound APCP. In 2009, a group succeeded in creating a propellant of water and nanoaluminium ( ALICE ). Typical HEC propellants start with a standard composite propellant mixture (such as APCP) and add a high-energy explosive to

1504-466: A sugar fuel (typically dextrose , sorbitol , or sucrose ) that are cast into shape by gently melting the propellant constituents together and pouring or packing the amorphous colloid into a mold. Candy propellants generate a low-medium specific impulse of roughly 130 s (1.3 km/s) and, thus, are used primarily by amateur and experimental rocketeers. DB propellants are composed of two monopropellant fuel components where one typically acts as

1598-684: A vacuum specific impulse ( I sp ) as high as 285.6 seconds (2.801 km/s) (Titan IVB SRMU). This compares to 339.3 s (3.327 km/s) for RP1/LOX (RD-180) and 452.3 s (4.436 km/s) for LH 2 /LOX (Block II RS-25 ) bipropellant engines. Upper stage specific impulses are somewhat greater: as much as 303.8 s (2.979 km/s) for APCP (Orbus 6E), 359 s (3.52 km/s) for RP1/LOX (RD-0124) and 465.5 s (4.565 km/s) for LH 2 /LOX (RL10B-2). Propellant fractions are usually somewhat higher for (non-segmented) solid propellant first stages than for upper stages. The 53,000-kilogram (117,000 lb) Castor 120 first stage has

1692-601: A very primitive form of solid-propellant rocket. Illustrations and descriptions in the 14th century Chinese military treatise Huolongjing by the Ming dynasty military writer and philosopher Jiao Yu confirm that the Chinese in 1232 used proto solid propellant rockets then known as " fire arrows " to drive back the Mongols during the Mongol siege of Kaifeng . Each arrow took a primitive form of

1786-435: Is a "poison-fog divine smoke eruptor," in which "blinding gunpowder" and "poisonous gunpowder" were packed into hollow shells used in burning the faces and eyes of enemies, along with choking them with a formidable spray of poisonous smoke. Cannons were mounted on frames or on wheeled carriages so that they could be rotated to change directions. The Huolongjing also contains a hand held organ gun with up to ten barrels. For

1880-409: Is a Chinese military treatise compiled and edited by Jiao Yu and Liu Bowen of the early Ming dynasty (1368–1683) during the 14th century. The Huolongjing is primarily based on the text known as Huolong Shenqi Tufa ( Illustrations of Divine Fire Dragon Engines ), which no longer exists. The Huolongjing' s intended function was to serve as a guide to "fire weapons" involving gunpowder during

1974-492: Is another pressed propellant that does not find any practical application outside specialized amateur rocketry circles due to its poor performance (as most ZS burns outside the combustion chamber) and fast linear burn rates on the order of 2 m/s. ZS is most often employed as a novelty propellant as the rocket accelerates extremely quickly leaving a spectacular large orange fireball behind it. In general, rocket candy propellants are an oxidizer (typically potassium nitrate) and

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2068-552: Is cheap and fairly easy to produce. The fuel grain is typically a mixture of pressed fine powder (into a solid, hard slug), with a burn rate that is highly dependent upon exact composition and operating conditions. The specific impulse of black powder is low, around 80 s (0.78 km/s). The grain is sensitive to fracture and, therefore, catastrophic failure. Black powder does not typically find use in motors above 40 newtons (9.0 pounds-force) thrust. Composed of powdered zinc metal and powdered sulfur (oxidizer), ZS or "micrograin"

2162-478: Is considered by some historians to be the ancestor of modern cluster munitions. Needham says that the written material and illustration of this rocket come from the oldest stratum of the Huolongjing , which can be dated to about 1300-1350 from the book's part 1, chapter 3, page 23. The fire lance or fire tube—a combination of a firearm and flamethrower —had been adapted and changed into several different forms by

2256-408: Is equal to the volumetric rate times the fuel density ρ {\displaystyle \rho } : Several geometric configurations are often used depending on the application and desired thrust curve : The casing may be constructed from a range of materials. Cardboard is used for small black powder model motors, whereas aluminium is used for larger composite-fuel hobby motors. Steel

2350-428: Is non-polluting: acid-free, solid particulates-free, and lead-free. It is also smokeless and has only a faint shock diamond pattern that is visible in the otherwise transparent exhaust. Without the bright flame and dense smoke trail produced by the burning of aluminized propellants, these smokeless propellants all but eliminate the risk of giving away the positions from which the missiles are fired. The new CL-20 propellant

2444-411: Is shock-insensitive (hazard class 1.3) as opposed to current HMX smokeless propellants which are highly detonable (hazard class 1.1). CL-20 is considered a major breakthrough in solid rocket propellant technology but has yet to see widespread use because costs remain high. Electric solid propellants (ESPs) are a family of high performance plastisol solid propellants that can be ignited and throttled by

2538-561: Is the Heilongjiang hand cannon , dated to 1288 using contextual evidence. The History of Yuan records that in that year a rebellion of the Christian Mongol prince Nayan broke out and the Jurchen commander Li Ting who, along with a Korean brigade conscripted by Kublai Khan , suppressed Nayan's rebellion using hand cannons and portable bombards . The predecessor of the metal barrel

2632-434: Is to achieve mid-course exo-atmospheric ABM capability from missiles small enough to fit in existing ship-based below-deck vertical launch tubes and air-mobile truck-mounted launch tubes. CL-20 propellant compliant with Congress' 2004 insensitive munitions (IM) law has been demonstrated and may, as its cost comes down, be suitable for use in commercial launch vehicles, with a very significant increase in performance compared with

2726-645: The Battle of Khalkhin Gol . In June 1938, the RNII began developing a multiple rocket launcher based on the RS-132 rocket. In August 1939, the completed product was the BM-13 / Katyusha rocket launcher . Towards the end of 1938 the first significant large scale testing of the rocket launchers took place, 233 rockets of various types were used. A salvo of rockets could completely straddle a target at

2820-414: The Huolongjing was called the 'lotus bunch' shot arrows accompanied by a fiery blast. In addition to fire lances, the Huolongjing also illustrates a tall, vertical, mobile shield used to hide and protect infantry, known as the "mysteriously moving phalanx -breaking fierce-flame sword-shield". This large, rectangular shield would have been mounted on wheels with five rows of six circular holes each where

2914-683: The Jurchen conquerors of Kaifeng City in 1126. An even earlier text, the Wujing Zongyao (武经总要, "Collection of the Most Important Military Techniques"), written in 1044 by Song scholars Zeng Gongliang and Yang Weide, described the use of three spring or triple bow arcuballista that fired arrow bolts holding gunpowder. Although written in 1630 (second edition in 1664), the Wulixiaoshi of Fang Yizhi said that fire arrows were presented to Emperor Taizu of Song in 960. Even after

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3008-560: The Polaris Sales Agreement . In 1982, the agreement was changed to supply Trident II instead. This article relating to missiles is a stub . You can help Misplaced Pages by expanding it . Solid-fuel rocket A solid-propellant rocket or solid rocket is a rocket with a rocket engine that uses solid propellants ( fuel / oxidizer ). The earliest rockets were solid-fuel rockets powered by gunpowder . The inception of gunpowder rockets in warfare can be credited to

3102-637: The Reactive Scientific Research Institute (RNII) with the development of the RS-82 and RS-132 rockets , including designing several variations for ground-to-air, ground-to-ground, air-to-ground and air-to-air combat. The earliest known use by the Soviet Air Force of aircraft-launched unguided anti-aircraft rockets in combat against heavier-than-air aircraft took place in August 1939 , during

3196-724: The Red Turban Rebellion and revolt against the Yuan dynasty , while the oldest material found in his text dates to 1280. Jiao Yu was a firearm manufacturer for the first Ming emperor, Zhu Yuanzhang , during the mid-14th century. He was eventually put in charge of the Shenjiying armoury where all the firearms were stored. A second and third volume to the Huolongjing known as Huolongjing Erji ( Fire Dragon Manual Volume Two ) and Huolongjing Sanji ( Fire Dragon Manual Volume Three ) were published in 1632 with content describing weapons such as

3290-746: The Second Anglo-Mysore War that ended in a humiliating defeat for the British East India Company . Word of the success of the Mysore rockets against the British triggered research in England, France, Ireland and elsewhere. When the British finally conquered the fort of Srirangapatana in 1799, hundreds of rockets were shipped off to the Royal Arsenal near London to be reverse-engineered. This led to

3384-500: The fuel and oxidizer mass. Grain geometry and chemistry are then chosen to satisfy the required motor characteristics. The following are chosen or solved simultaneously. The results are exact dimensions for grain, nozzle, and case geometries: The grain may or may not be bonded to the casing. Case-bonded motors are more difficult to design, since the deformation of the case and the grain under flight must be compatible. Common modes of failure in solid rocket motors include fracture of

3478-541: The musket and breech-loading cannons. After the end of the Ming dynasty , the Qing dynasty outlawed reprinting of the Huolongjing for using expressions such as 'northern barbarians,' which offended the ruling Manchu elite. Although its destructive force was widely recognized by the 11th century, gunpowder continued to be known as a "fire-drug" (huo yao) because of its original intended pharmaceutical properties. However soon after

3572-490: The wheellock , and the advent of the flintlock musket of the 17th century, they surpassed the level of earlier Chinese firearms. Illustrations of Ottoman and European riflemen with detailed illustrations of their weapons appeared in Zhao Shizhen's book Shenqipu of 1598, and Ottoman and European firearms were held in great esteem. However, by the 17th century Đại Việt had also been manufacturing muskets of their own, which

3666-432: The "divine rocket-arrow block". Rockets described in the Huolongjing were not all in the shape of standard fire arrows and some had artificial wings attached. An illustration shows that fins were used to increase aerodynamic stability for the flight path of the rocket, which according to Jiao Yu could rise hundreds of feet before landing at the designated enemy target. The Huolongjing also describes and illustrates

3760-536: The "match-holding lance gun" (chi huo–sheng qiang), it described its arrangement as a match brought down to the touch hole of three gun barrels, one after the other. During the reign of the Yongle Emperor (1402–1424), the Shenjiying , a specialized military body, was in part a cavalry force that utilized tubes filled with inflammable materials holstered to their sides, and also a firearm infantry division that handled light artillery and their transportation, including

3854-424: The 'submarine dragon–king' is made of wrought iron, and carried on a (submerged) wooden board, [appropriately weighted with stones]. The (mine) is enclosed in an ox-bladder. Its subtlety lies in the fact that a thin incense(–stick) is arranged (to float) above the mine in a container. The (burning) of this joss stick determines the time at which the fuse is ignited, but without air its glowing would of course go out, so

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3948-485: The 1280s to 1350s. Its predecessor, the Huolong Shenqi Tufa (Fire-Drake Illustrated Technology of Magically (Efficacious) Weapons), has since been lost. The Huolongjing was one of three early Ming military treatises that were mentioned by Jiao Xu, but only the Huolongjing remains. Although the earliest edition of the Huolongjing was written by Jiao Yu, a Ming general, sometime between 1360-1375, its preface

4042-570: The 2010s include the European Ariane 5 , US Atlas V and Space Shuttle , and Japan's H-II . The largest solid rocket motors ever built were Aerojet's three 6.60-meter (260 in) monolithic solid motors cast in Florida. Motors 260 SL-1 and SL-2 were 6.63 meters (261 in) in diameter, 24.59 meters (80 ft 8 in) long, weighed 842,900 kilograms (1,858,300 lb), and had a maximum thrust of 16 MN (3,500,000 lbf). Burn duration

4136-655: The Athena IC and IIC commercial launch vehicles. A four-stage Athena II using Castor 120s as both first and second stages became the first commercially developed launch vehicle to launch a lunar probe ( Lunar Prospector ) in 1998. Solid rockets can provide high thrust for relatively low cost. For this reason, solids have been used as initial stages in rockets (for example the Space Shuttle ), while reserving high specific impulse engines, especially less massive hydrogen-fueled engines, for higher stages. In addition, solid rockets have

4230-529: The Ming considered to be superior to both European and Ottoman firearms, including Japanese imports as well. Vietnamese firearms were copied and disseminated throughout China in quick order. The 16th-century breech-loading model entered China around 1517 when Fernão Pires de Andrade arrived in China. However, he and the Portuguese embassy were rejected as problems in Ming-Portuguese relations were exacerbated when

4324-439: The Ming wars. Chinese cannon development reached internal maturity with the muzzle loading wrought iron "great general cannon" (大將軍炮), otherwise known by its heavier variant name "great divine cannon" (大神銃), which could weigh up to 600 kg (1,300 lb) and was capable of firing several iron balls and upward of a hundred iron shots at once. The lighter "great general cannon" weighed up to 360 kg (790 lb) and could fire

4418-465: The Mongols in 1259, the official Li Zengbo wrote in his Ko Zhai Za Gao, Xu Gao Hou that the city of Qingzhou was manufacturing one to two thousand strong iron-cased bomb shells a month, and delivered them to Xiangyang and Yingzhou in loads of about ten to twenty thousand shells at a time. The Huolongjing' s primary contribution to gunpowder was in expanding its role as a chemical weapon. Jiao Yu proposed several gunpowder compositions in addition to

4512-501: The Song dynasty. In China, gunpowder weapons underwent significant technological changes which resulted in a vast array of weapons that eventually led to the cannon. The cannon's first confirmed use occurred during the Mongol Yuan dynasty in a suppression of rebel forces by Yuan Jurchen forces armed with hand cannons. Cannon development continued into the Ming and saw greater proliferation during

4606-441: The Song prohibited the populaces of Hedong ( Shanxi ) and Hebei from selling sulphur and saltpetre to foreigners. In 1132 gunpowder was referred to specifically for its military values for the first time and was called "fire bomb medicine" rather than "fire medicine". While Chinese gunpowder formulas by the late 12th century and at least 1230 were powerful enough for explosive detonations and bursting cast iron shells, gunpowder

4700-493: The aid of a curative additive. Because of its high performance, moderate ease of manufacturing, and moderate cost, APCP finds widespread use in space, military, and amateur rockets, whereas cheaper and less efficient ANCP finds use in amateur rocketry and gas generators . Ammonium dinitramide , NH 4 N(NO 2 ) 2 , is being considered as a 1-to-1 chlorine-free substitute for ammonium perchlorate in composite propellants. Unlike ammonium nitrate, ADN can be substituted for AP without

4794-410: The air cannot escape the effects of the explosion". Explosive devices include the "flying-sand divine bomb releasing ten thousand fires", which consisted of a tube of gunpowder placed in an earthenware pot filled with quicklime , resin, and alcoholic extracts of poisonous plants. Jiao Yu called the earliest fire arrows shot from bows (not rocket launchers) "fiery pomegranate shot from a bow" because

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4888-1310: The ancient Chinese, and in the 13th century, the Mongols played a pivotal role in facilitating their westward adoption. All rockets used some form of solid or powdered propellant until the 20th century, when liquid-propellant rockets offered more efficient and controllable alternatives. Because of their simplicity and reliability, solid rockets are still used today in military armaments worldwide, model rockets , solid rocket boosters and on larger applications. Since solid-fuel rockets can remain in storage for an extended period without much propellant degradation, and since they almost always launch reliably, they have been frequently used in military applications such as missiles . The lower performance of solid propellants (as compared to liquids) does not favor their use as primary propulsion in modern medium-to-large launch vehicles customarily used for commercial satellites and major space probes. Solids are, however, frequently used as strap-on boosters to increase payload capacity or as spin-stabilized add-on upper stages when higher-than-normal velocities are required. Solid rockets are used as light launch vehicles for low Earth orbit (LEO) payloads under 2 tons or escape payloads up to 500 kilograms (1,100 lb). A simple solid rocket motor consists of

4982-459: The application of electric current. Unlike conventional rocket motor propellants that are difficult to control and extinguish, ESPs can be ignited reliably at precise intervals and durations. It requires no moving parts and the propellant is insensitive to flames or electrical sparks. Solid propellant rocket motors can be bought for use in model rocketry ; they are normally small cylinders of black powder fuel with an integral nozzle and optionally

5076-454: The cannon, called the "eruptor", as a cast bronze device which had an average length of 53 inches (130 cm). He wrote that some cannons were simply filled with about 100 lead balls, but others, called the "flying-cloud thunderclap eruptor" (飞云霹雳炮; feiyun pili pao) had large rounds that produced a bursting charge upon impact. The ammunition consisted of hollow cast iron shells packed with gunpowder to create an explosive effect. Also mentioned

5170-460: The cargo bay of the Space Shuttle. Star motors have propellant fractions as high as 94.6% but add-on structures and equipment reduce the operating mass fraction by 2% or more. Higher performing solid rocket propellants are used in large strategic missiles (as opposed to commercial launch vehicles). HMX , C 4 H 8 N 4 (NO 2 ) 4 , a nitramine with greater energy than ammonium perchlorate,

5264-452: The casing is often implemented, which ablates to prolong the life of the motor casing. A convergent-divergent design accelerates the exhaust gas out of the nozzle to produce thrust. The nozzle must be constructed from a material that can withstand the heat of the combustion gas flow. Often, heat-resistant carbon-based materials are used, such as amorphous graphite or reinforced carbon–carbon . Some designs include directional control of

5358-404: The chemical formula for gunpowder was recorded in the Wujing Zongyao of 1044, evidence of state interference in gunpowder affairs began appearing. Realizing the military applications of gunpowder, the Song court banned private transactions involving sulphur and saltpeter in 1067 despite the widespread use of saltpeter as a flavor enhancer, and moved to monopolize gunpowder production. In 1076

5452-409: The container is connected with the mine by a (long) piece of goat's intestine (through which passes the fuse). At the upper end the (joss stick in the container) is kept floating by (an arrangement of) goose and wild–duck feathers, so that it moves up and down with the ripples of the water. On a dark (night) the mine is sent downstream (towards the enemy's ships), and when the joss stick has burnt down to

5546-454: The currently favored APCP solid propellants. With a specific impulse of 309 s already demonstrated by Peacekeeper's second stage using HMX propellant, the higher energy of CL-20 propellant can be expected to increase specific impulse to around 320 s in similar ICBM or launch vehicle upper stage applications, without the explosive hazard of HMX. An attractive attribute for military use is the ability for solid rocket propellant to remain loaded in

5640-611: The exhaust can turn the smoke opaque. A powdered oxidizer and powdered metal fuel are intimately mixed and immobilized with a rubbery binder (that also acts as a fuel). Composite propellants are often either ammonium-nitrate -based (ANCP) or ammonium-perchlorate -based (APCP). Ammonium nitrate composite propellant often uses magnesium and/or aluminium as fuel and delivers medium performance (I sp of about 210 s (2.1 km/s)) whereas ammonium perchlorate composite propellant often uses aluminium fuel and delivers high performance: vacuum I sp up to 296 s (2.90 km/s) with

5734-531: The exhaust. This can be accomplished by gimballing the nozzle, as in the Space Shuttle SRBs, by the use of jet vanes in the exhaust as in the V-2 rocket, or by liquid injection thrust vectoring (LITV). LITV consists of injecting a liquid into the exhaust stream after the nozzle throat. The liquid then vaporizes, and in most cases chemically reacts, adding mass flow to one side of the exhaust stream and thus providing

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5828-544: The fire lances could be placed. The shield itself would have been accompanied by swordsmen on either side to protect the gunmen. In China, the first cannon-barrel design portrayed in artwork was a stone sculpture dated to 1128 found in Sichuan province. The oldest extant cannon containing an inscription is a bronze cannon of China inscribed with the date, "2nd year of the Dade era, Yuan dynasty" (1298). The oldest confirmed extant cannon

5922-554: The first industrial manufacture of military rockets with the Congreve rocket in 1804. In 1921 the Soviet research and development laboratory Gas Dynamics Laboratory began developing solid-propellant rockets, which resulted in the first launch in 1928, that flew for approximately 1,300 metres. These rockets were used in 1931 for the world's first successful use of rockets to assist take-off of aircraft . The research continued from 1933 by

6016-445: The functional definition of double base propellants. One of the most active areas of solid propellant research is the development of high-energy, minimum-signature propellant using C 6 H 6 N 6 (NO 2 ) 6 CL-20 nitroamine ( China Lake compound #20), which has 14% higher energy per mass and 20% higher energy density than HMX. The new propellant has been successfully developed and tested in tactical rocket motors. The propellant

6110-485: The fuse, there is a great explosion. In the later Tiangong Kaiwu (The Exploitation of the Works of Nature) treatise, written by Song Yingxing in 1637, the ox bladder described by Jiao Yu is replaced with a lacquer bag and a cord pulled from a hidden ambusher located on the nearby shore, which would release a flint steel–wheel firing mechanism to ignite the fuse of the naval mine. Gunpowder warfare occurred in earnest during

6204-470: The gooey asphalt, creating a flexible but geometrically stable load-bearing propellant grain that bonded securely to the motor casing. This made possible much larger solid rocket motors. Atlantic Research Corporation significantly boosted composite propellant I sp in 1954 by increasing the amount of powdered aluminium in the propellant to as much as 20%. Solid-propellant rocket technology got its largest boost in technical innovation, size and capability with

6298-440: The grain, failure of case bonding, and air pockets in the grain. All of these produce an instantaneous increase in burn surface area and a corresponding increase in exhaust gas production rate and pressure, which may rupture the casing. Another failure mode is casing seal failure. Seals are required in casings that have to be opened to load the grain. Once a seal fails, hot gas will erode the escape path and result in failure. This

6392-402: The handling of gun carriages. The first recorded use of land mines occurred in 1277 when officer Lou Qianxia of the late Song dynasty , who is credited with their invention, used them to kill Mongol soldiers. Jiao Yu wrote that land mines were spherical, made of cast iron, and their fuses were ignited by the enemy movement disturbing a trigger mechanism. Although his book did not elaborate on

6486-658: The ingredients necessary for combustion within the chamber in which they are burned. More advanced solid rocket motors can be throttled , or extinguished and re-ignited, by control of the nozzle geometry or through the use of vent ports. Further, pulsed rocket motors that burn in segments, and that can be ignited upon command are available. Modern designs may also include a steerable nozzle for guidance, avionics , recovery hardware ( parachutes ), self-destruct mechanisms, APUs , controllable tactical motors, controllable divert and attitude control motors, and thermal management materials. The medieval Song dynasty Chinese invented

6580-413: The late Southern Song dynasty (1127–1279). From the section of the oldest passages in the Huolongjing , the text reads: One uses a bamboo stick 4 ft 2 in long, with an iron (or steel) arrow–head 4.5 in long...behind the feathering there is an iron weight 0.4 in long. At the front end there is a carton tube bound on to the stick, where the 'rising gunpowder' is lit. When you want to fire it off, you use

6674-401: The lump of gunpowder–filled paper wrapped around the arrow below the metal arrowhead resembled the shape of a pomegranate . He advised that a piece of hemp cloth should be used to strengthen the wad of paper and sealed with molten pine resin . Although he described the fire arrow in great detail, it was mentioned by the much earlier Xia Shaozeng, when 20,000 fire arrows were handed over to

6768-463: The mines are connected by fuses through the gunpowder fire-ducts, and all originate from a steel wheel (gang lun). This must be well concealed from the enemy. On triggering the firing device the mines will explode, sending pieces of iron flying in all directions and shooting up flames towards the sky. For the use of naval mines, he wrote of slowly burning joss sticks that were disguised and timed to explode against enemy ships nearby: The sea–mine called

6862-401: The mines' fuses underground. The explosive mine is made of cast iron about the size of a rice-bowl, hollow inside with (black) powder rammed into it. A small bamboo tube is inserted and through this passes the fuse, while outside (the mine) a long fuse is led through fire-ducts. Pick a place where the enemy will have to pass through, dig pits and bury several dozen such mines in the ground. All

6956-685: The mix). Almost all sounding rockets use solid motors. Due to reliability, ease of storage and handling, solid rockets are used on missiles and ICBMs. Solid rockets are suitable for launching small payloads to orbital velocities, especially if three or more stages are used. Many of these are based on repurposed ICBMs. Huolongjing The Huolongjing ( traditional Chinese : 火龍經 ; simplified Chinese : 火龙经 ; pinyin : Huǒ Lóng Jīng ; Wade-Giles : Huo Lung Ching ; rendered in English as Fire Drake Manual or Fire Dragon Manual ), also known as Huoqitu (“Firearm Illustrations”),

7050-560: The mix. This extra component usually is in the form of small crystals of RDX or HMX , both of which have higher energy than ammonium perchlorate. Despite a modest increase in specific impulse, implementation is limited due to the increased hazards of the high-explosive additives. Composite modified double base propellants start with a nitrocellulose/nitroglycerin double base propellant as a binder and add solids (typically ammonium perchlorate (AP) and powdered aluminium ) normally used in composite propellants. The ammonium perchlorate makes up

7144-420: The next 50 years. By the later 1980s and continuing to 2020, these government-developed highly-capable solid rocket technologies have been applied to orbital spaceflight by many government-directed programs , most often as booster rockets to add extra thrust during the early ascent of their primarily liquid rocket launch vehicles . Some designs have had solid rocket upper stages as well. Examples flying in

7238-454: The oldest known multistage rocket ; this was the "fire-dragon issuing from the water" (huo long chu shui), which was known to be used by the Chinese navy. It was a two-stage rocket that had carrier or booster rockets that would automatically ignite a number of smaller rocket arrows that were shot out of the front end of the missile, which was shaped like a dragon's head with an open mouth, before eventually burning out. This multistage rocket

7332-557: The oxygen deficit introduced by using nitrocellulose , improving the overall specific impulse. The aluminium improves specific impulse as well as combustion stability. High performing propellants such as NEPE-75 used to fuel the Trident II D-5 SLBM replace most of the AP with polyethylene glycol -bound HMX , further increasing specific impulse. The mixing of composite and double base propellant ingredients has become so common as to blur

7426-463: The propellant surface area exposed to the combustion gases. Since the propellant volume is equal to the cross sectional area A s {\displaystyle A_{s}} times the fuel length, the volumetric propellant consumption rate is the cross section area times the linear burn rate b ˙ {\displaystyle {\dot {b}}} , and the instantaneous mass flow rate of combustion gases generated

7520-417: The retired Peacekeeper ICBMs). The Naval Air Weapons Station at China Lake, California, developed a new compound, C 6 H 6 N 6 (NO 2 ) 6 , called simply CL-20 (China Lake compound 20). Compared to HMX, CL-20 has 14% more energy per mass, 20% more energy per volume, and a higher oxygen-to-fuel ratio. One of the motivations for development of these very high energy density military solid propellants

7614-403: The rocket for long durations and then be reliably launched at a moment's notice. Black powder (gunpowder) is composed of charcoal (fuel), potassium nitrate (oxidizer), and sulfur (fuel and catalyst). It is one of the oldest pyrotechnic compositions with application to rocketry. In modern times, black powder finds use in low-power model rockets (such as Estes and Quest rockets), as it

7708-635: The rocket was invented in China the fire arrow was never entirely phased out: it saw use in the Second Opium War when Chinese used fire arrows against the French in 1860. By the time of Jiao Yu, the term "fire arrow" had taken on a new meaning and also referred to the earliest rockets found in China. The simple transition of this was to use a hollow tube instead of a bow or ballista firing gunpowder-impregnated fire arrows. The historian Joseph Needham wrote that this discovery came sometime before Jiao Yu during

7802-455: The standard potassium nitrate (saltpetre), sulphur, and charcoal. Described are the military applications of "divine gunpowder", "poison gunpowder", and "blinding and burning gunpowder." Poisonous gunpowder for hand-thrown or trebuchet launched bombs was created using a mixture of tung oil , urine, sal ammoniac , feces, and scallion juice heated and coated upon tiny iron pellets and broken porcelain. According to Jiao Yu, "even birds flying in

7896-530: The time Jiao Yu edited the Huolongjing . The earliest depiction of a fire lance is dated c. 950, a Chinese painting on a silk banner found at the Buddhist site of Dunhuang . These early fire lances were made of bamboo tubes, but metal barrels had appeared during the 13th century, and shot gunpowder flames along with "coviative" projectiles such as small porcelain shards or metal scraps. The first metal barrels were not designed to withstand high-nitrate gunpowder and

7990-460: The trigger mechanism, it does mention the use of steel wheels as the trigger mechanism. The earliest illustration and description of the "steel wheel" mechanism was the Binglu of 1606. According to it, the steel wheel trigger mechanism utilized a pin release, dropping weights, cords and axles that worked to rotate a spinning "steel wheel" that rotated against a piece of flint to provide sparks that ignited

8084-610: The various mid-20th century government initiatives to develop increasingly capable military missiles. After initial designs of ballistic missile military technology designed with liquid-propellant rockets in the 1940s and 1950s, both the Soviet Union and the United States embarked on major initiatives to develop solid-propellant local , regional , and intercontinental ballistic missiles, including solid-propellant missiles that could be launched from air or sea . Many other governments also developed these military technologies over

8178-480: Was fired. An illustration of this appears in the Huolongjing , and a description of its effectiveness in obfuscating the location of the rockets from the enemy is provided. The Huolongjing also describes and illustrates two kinds of mounted rocket launchers that fired multiple rockets. There was a cylindrical, basket-work rocket launcher called the "Mr. Facing-both-ways rocket arrow firing basket", as well as an oblong-section, rectangular, box rocket launcher known as

8272-423: Was made more potent by applying the enrichment of sulphur from pyrite extracts. Chinese gunpowder solutions reached maximum explosive potential in the 14th century and at least six formulas are considered to have been optimal for creating explosive gunpowder, with levels of nitrate ranging from 12% to 91%. Evidence of large scale explosive gunpowder weapons manufacturing began to appear. While engaged in war with

8366-449: Was made of bamboo, which was recorded in use by a Chinese garrison commander at Anlu , Hubei province, in the year 1132. One of the earliest references to the destructive force of a cannon in China was made by Zhang Xian in 1341, with his verse known as The Iron Cannon Affair . Zhang wrote that its cannonball could "pierce the heart or belly when it strikes a man or horse, and can even transfix several persons at once". Jiao Yu describes

8460-595: Was not provided until the Nanyang publication of 1412. The 1412 edition, known as Huolongjing Quanji ( Complete Collection of the Fire Dragon Manual ), remains largely unchanged from its predecessor with the exception of its preface, which provides an account of Jiao Yu's time in the Hongwu Emperor 's army. In the preface Jiao Yu claims to describe gunpowder weapons that had seen use since 1355 during his involvement in

8554-478: Was the cause of the Space Shuttle Challenger disaster . Solid rocket fuel deflagrates from the surface of exposed propellant in the combustion chamber. In this fashion, the geometry of the propellant inside the rocket motor plays an important role in the overall motor performance. As the surface of the propellant burns, the shape evolves (a subject of study in internal ballistics), most often changing

8648-423: Was two minutes. The nozzle throat was large enough to walk through standing up. The motor was capable of serving as a 1-to-1 replacement for the 8-engine Saturn I liquid-propellant first stage but was never used as such. Motor 260 SL-3 was of similar length and weight but had a maximum thrust of 24 MN (5,400,000 lbf) and a shorter duration. Design begins with the total impulse required, which determines

8742-407: Was used for the space shuttle boosters . Filament-wound graphite epoxy casings are used for high-performance motors. The casing must be designed to withstand the pressure and resulting stresses of the rocket motor, possibly at elevated temperature. For design, the casing is considered a pressure vessel . To protect the casing from corrosive hot gases, a sacrificial thermal liner on the inside of

8836-642: Was used in the propellant of the Peacekeeper ICBM and is the main ingredient in NEPE-75 propellant used in the Trident II D-5 Fleet Ballistic Missile. It is because of explosive hazard that the higher energy military solid propellants containing HMX are not used in commercial launch vehicles except when the LV is an adapted ballistic missile already containing HMX propellant (Minotaur IV and V based on

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