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41-583: Various programs such as Equatorial ElectroJet (EEJ), Leonid Meteor Shower (LMS), Indian Middle Atmosphere Programme (IMAP), Monsoon Experiment (MONEX), Middle Atmosphere Dynamics (MIDAS), and Sooryagrahan-2010 have been conducted using the Rohini sounding rocket series. It has been the forerunners for ISRO's heavier and more complex launch vehicles, with continued usage even today for atmospheric and meteorological experiment and research. Currently, three versions are offered as operational sounding rockets , which cover

82-481: 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

123-574: A M5 Nike rocket booster for its first stage by Aerolab, the Nike-Apache sounding rocket was capable of lifting 100 pounds (45 kg) of instruments to an apogee of 100 miles (160 km). The first launch of Nike-Apache was conducted by the United States Air Force on 17 February 1961. Popular due to its low cost (US$ 6,000) and ability to be fired from many locales, 636 launches were conducted between 1961 and 1978, with

164-536: A Sounding Rocket such as the Nike-Apache may deposit sodium clouds to observe very high altitude winds. Larger, higher altitude rockets have multiple stages to increase altitude and/or payload capability. The freefall part of the flight is an elliptic trajectory with vertical major axis allowing the payload to appear to hover near its apogee . The average flight time is less than 30 minutes; usually between five and 20 minutes. The rocket consumes its fuel on

205-566: A payload range of 8-100 Kg and an apogee range of 80-475 km. Several scientific missions with national and international participation have been conducted using the Rohini sounding rockets. On November 21, 1963, the American Nike-Apache was the first sounding rocket to launch from Thumba. Following that, two-stage rockets from France (Centaure) and Russia (M-100) were launched. In 1967, the Rohini RH-75, an ISRO variant,

246-638: A small Liquid-propellant rocket to provide the GALCIT team necessary experience to aid in developing the Corporal missile. Malina with Tsien Hsue-shen ( Qian Xuesen in Pinyin transliteration), wrote "Flight analysis of a Sounding Rocket with Special Reference to Propulsion by Successive Impulses." As the Signal Corps rocket was being developed for the Corporal project, and lacked any guidance mechanism, it

287-511: A sounding rocket also makes launching from temporary sites possible, allowing field studies at remote locations, and even in the middle of the ocean, if fired from a ship. Weather observations, up to an altitude of 75 km, are done with rocketsondes , a kind of sounding rocket for atmospheric observations that consists of a rocket and radiosonde . The sonde records data on temperature , moisture , wind speed and direction, wind shear , atmospheric pressure , and air density during

328-556: A survey or a poll". Sounding in the rocket context is equivalent to "taking a measurement". The basic elements of a modern sounding rocket are a solid-fuel rocket motor and a science payload . In certain Sounding Rockets the payload may even be nothing more than a smoke trail as in the Nike Smoke which is used to determine wind directions and strengths more accurately than may be determined by weather balloons . Or

369-1065: Is a modified version of RH-560. The RH-200 is used for meteorological studies, the RH-300 Mk-II for Middle atmospheric studies and the RH-560 Mk-II for Upper atmospheric studies and ionospheric studies. The RH-200 was used as the rocket for the first payload launch in India made by students of VIT University in Vellore . (71 lb) (4.90 ft) (0.3 inch) (6.2 mi) (34 mi) (88 lb) (8.20 ft) (0.39 ft) (1,798 lbf) (12 mi) (220 lb) (11.80 ft) (0.65 ft) (3,821 lbf) (50 mi) (660 lb) (13.40 ft) (1.01 ft) (8,542 lbf) (62 mi) (1,100 lb) (19.30 ft) (1.01 ft) (8,767 lbf) (72 mi) (2,800 lb) (27.50 ft) (1.83 ft) (17,085 lbf) (250 mi) (3,530 lb) (29.80 ft) (1.83 ft) (17,085 lbf) (341 mi) (317 mi) Nike-Apache The Nike Apache , also known as Argo B-13 ,

410-490: The RH-300 Mk-II , has a maximum launch altitude of 116 kilometres (72 mi). It has ability to lift a payload up to 80 kilograms (20 kg of scientific payload) having volume measuring 380*500 mm in diameter. It is capable of reaching very high acceleration (20 G to M6). Numerous payloads can be tested in a single flight. This two stage vehicle is derived from French Stromboli engine technology. Another variant,

451-524: The RH-560 Mk-II , can reach a maximum launch altitude of 548 kilometres (341 mi). The RH-560 Mk-III variant's maiden flight (the flight was successful) was 12 March 2021. It achieved an apogee of 511.73 kms against the pre-flight prediction of 476 kms. The payloads were Electron and Neutral Wind Probe (ENWi), Langmuir Probe (LP) and Tri Methyl Aluminium (TMA). On 23rd July 2024, ISRO successfully launched world's first air breathing rocket which

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492-584: The Veronique (rocket) was began in 1949, it was not until 1952 that the first full scale Veronique was launched. Veronique variants were flown until 1974. The Monica (rocket) family, an all solid fueled which was pursued in a number of versions and later replaced by the ONERA. series of rockets. Japan was another early user with the Kappa (rocket) . Japan also pursued Rockoons. The People's Republic of China

533-844: The WAC Corporal , Aerobee , and Viking . The German V-2 served both the US and the USSR's R-1 missile as sounding rockets during the immediate Post World War II periods. During the 1950s and later the inexpensive availability of surplus military boosters such as those used by the Nike , Talos , Terrier , and Sparrow . Since the 1960s designed for the purpose rockets such as the Black Brant series have dominated sounding rockets, though often having additional stages, many from military surplus. The earliest attempts at developing Sounding Rockets were in

574-473: The exoatmospheric region between 97 and 201 km (60 and 125 miles). The origin of the term comes from nautical vocabulary to sound , which is to throw a weighted line from a ship into the water to measure the water's depth. The term itself has its etymological roots in the Romance languages word for probe , of which there are nouns sonda and sonde and verbs like sondear which means "to do

615-443: The first stage of the rising part of the flight, then often separates and falls away, leaving the payload to complete the arc, sometimes descending under a drag source such as a small balloon or a parachute . Sounding rockets have utilized balloons, airplanes and artillery as "first stages." Project Farside utilized a Rockoon composed of a 106,188-m3 (3,750-ft3) balloon, lifting a four stage rocket composed of 4 Recrute rockets as

656-785: The Aerobee ultimately powered the second stage of the Vanguard (rocket) , the first designed for the purpose Satellite Launch Vehicle , Vanguard. The AJ10 engine used by many Aerobees eventually evolved into the AJ10-190 which formed the Orbital Maneuvering System of the Space Shuttle. The Viking (rocket) was intended from the start by the Navy not only to be a sounding rocket capable of replacing, even exceeding

697-522: The RH-200. A polyvinyl chloride ( PVC )-based propellant had previously been employed with the RH-200 rocket. In September 2020, a new propellant based on hydroxyl-terminated polybutadiene ( HTPB ) was successfully used to launch it from the TERLS. The RH-300 is a single stage sounding rocket, derived from French Belier rocket engine technology. It has a launch altitude of 100 km (62 mi). A variant,

738-635: The Soviet Union. While all of the early rocket developers were concerned largely with developing the ability to launch rockets some had the objective of investigating the stratosphere and beyond. The All-Union Conference on the Study of Stratosphere was held in Leningrad (now St. Petersburg) in 1936. While the conference primarily dealt with balloon Radiosondes , there was a small group of rocket developers who sought to develop "recording rockets" to explore

779-619: The U.S.S.R in Moscow designed the R-06 which eventually flew but not in the meteorological role. The early Soviet efforts to develop a sounding rocket were the earliest efforts to develop a sounding rocket and ultimately failed before WWII. P. I. Ivanov built a three-stage which flew in March 1946. At the end of summer 1946 development ended because it lacked sufficient thrust to loft a sufficient research payload. The first successful sounding rocket

820-833: The V-2, but also to advance guided missile technology. The Viking was controlled by a multi-axis guidance system with gimbled Reaction Motors XLR10-RM-2 engine. The Viking was developed through two major versions. After the United States announced it intended to launch a satellite in the International Geophysical Year (1957-1958) the Viking was chosen as the first stage of the Vanguard Satellite Launch Vehicle. The last two Vikings were fired as Vanguard Test Vehicle 1 and 2. During

861-507: The final launch of a Nike-Apache taking place in September 1978. The Nike Apache was used to carry a variety of payloads to study a wide range of topics including radio astronomy, meteorology, aeronomy , atmospheric conditions, plasma physics, and solar physics. NASA flew them from Brazil, Canada, India, Norway, Pakistan, Spain, Suriname, Sweden, all across the US, and off of the converted escort carrier USNS  Croatan . Nike Apache

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902-493: The first stage with 1 Recruit as the second stage, with 4 Arrow II motors composing the third stage and finally a single Arrow II as the fourth stage. Sparoair , air launched from Navy F4D and F-4 fighters were examples of air launched sounding rockets. There were also examples of artillery launched sounding rockets including Project HARP 's 5", 7", and 15" guns, sometimes having additional Martlet rocket stages. The earliest Sounding Rockets were liquid propellant rockets such as

943-574: The first successful Sounding Rocket the WAC Corporal . By the early 1960s the Sounding Rocket was established technology. Sounding rockets are advantageous for some research because of their low cost, relatively short lead time (sometimes less than six months) and their ability to conduct research in areas inaccessible to either balloons or satellites. They are also used as test beds for equipment that will be used in more expensive and risky orbital spaceflight missions. The smaller size of

984-521: The flight. Position data ( altitude and latitude / longitude ) may also be recorded. Common meteorological rockets are the Loki and Super Loki , typically 3.7 m tall and powered by a 10 cm diameter solid fuel rocket motor . The rocket motor separates at an altitude of 1500 m and the rest of the rocketsonde coasts to apogee (highest point). This can be set to an altitude of 20 km to 113 km. Sounding rockets are commonly used for: Due to

1025-664: The high military relevance of ballistic missile technology, there has always been a close relationship between sounding rockets and military missiles. It is a typical dual-use technology , which can be used for both civil and military purposes. During the Cold War , the Federal Republic of Germany cooperated on this topic with countries that had not signed the Non-Proliferation Treaty on Nuclear Weapons at that time, such as Brazil, Argentina and India. In

1066-536: The magnetosphere, ionosphere, thermosphere and mesosphere. Sounding rockets have been used for the examination of atmospheric nuclear tests by revealing the passage of the shock wave through the atmosphere. In more recent times Sounding Rockets have been used for other nuclear weapons research. 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

1107-421: 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. For certain purposes Sounding Rockets may be flown to altitudes as high as 3,000 kilometers to allow observing times of around 40 minutes to provide geophysical observations of

1148-558: The post WWII era the USSR also pursued V-2 base sounding rockets. The last two R-1As were flown in 1949 as sounding rockets. They were followed between July 1951 and June 1956 by 4 R-1B, 2 R-1V, 3 R-1D and 5 R-1Es, and 1 R-1E (A-1). The improved V-2 descendant the R-2A could reach 120 miles and were flown between April 1957 and May 1962. Fifteen R-5Vs were flown from June 1965 to October 1983. Two R-5 VAOs were flown in September 1964 and October 1965. The first solid-fueled Soviet sounding rocket

1189-748: The results. After the start of WWII the CIT rocketry enthusiast found themselves involved in a number of defense programs, one of which, deemed Corporal, was intended to produce a bombardment guided missile the Corporal. Eventually known as the MGM-5 Corporal it became the first guided missile deployed by the US Army. During WWII the Signal Corps created a requirement for a sounding rocket to carry 25 pounds (11 kg) of instruments to 100,000 feet (30 km) or higher. To meet that goal Malina proposed

1230-643: The stratosphere and beyond. Amongst the speakers at the conference was Sergey Korolev who later became the leading figure of the Soviet space program. Specifically interested in sounding rocket design were V. V. Razumov, of the Leningrad Group for the Study of Jet Propulsion. A. I. Polyarny working in a special group within the Society for Assistance to the Defense, Aviation and Chemical Construction of

1271-781: The upper stage of the first two staged rocket the RTV-G-4 Bumper . Captured V-2s dominated American sounding rockets and other rocketry developments during the late 1940s. To meet the need for replacement a new sounding rocket was developed by the Aerojet Corporation to meet a requirement of the Applied Physics Laboratory and the Naval Research Laboratory . Over 1,000 Aerobees of various versions for varied customers were flow between 1947 and 1985. One engine produced for

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1312-676: Was Without Attitude Control. Thus it was named the WAC Corporal . The WAC Corporal served as the foundation of Sounding Rocketry in the USA. WAC Corporal was developed in two versions the second of which was much improved. After the war the WAC Corporal was in competition for sounding mission funding with the much larger captured V-2 rocket being tested by the U.S. Army. WAC Corporal was overshadowed at its job of cost-effectively lifting pounds of experiments to altitude, thus it effectively became obsolescent. WAC Corporals were later modified to become

1353-521: Was a single-stage solid-fuel rocket that was capable of carrying its payload up to an altitude of 55 km or more. When paired with a 650mm long by 40mm wide copper shaft dart used for meteorological research, it was referred to as a Menaka-I rocket. This rocket was launched on October 9, 1971, from Sriharikota. It was a single-stage rocket using a solid propellant , carrying a 7 kilograms (15 lb) payload to 19 kilometres (12 mi) in altitude. It flew twice between January 1970 and October 1971. It

1394-533: Was a two-stage sounding rocket developed by Aerolab , later Atlantic Research , for use by the United States Air Force and NASA . It became the standard NASA sounding rocket and was launched over 600 times between 1961 and 1978. The TE-307-2 Apache rocket motor was developed by Thiokol as an improvement of its Cajun series of rockets; the Apache was similar in appearance to Cajun, but had an improved propellant that allowed for better performance. Combined with

1435-548: Was created at the California Institute of Technology , where before World War II there was a group of rocket enthusiasts led by Frank Malina , under the aegis of Theodore von Kármán , known amidst the people of the CIT as the "Suicide Squad." The immediate goal of the Suicide Squad was exploring the upper atmosphere which required developing the means of lofting instruments to high altitude and recovering

1476-504: Was launched. The Rohini Sounding Rocket (RSR) Programme was established in 1975 to encompass all sounding rocket operations. The rockets in the series are designated with the letters RH (for "Rohini"), followed by a number corresponding to the diameter (in millimetres) of the rocket. The RH-75, the first sounding rocket developed by India, It weighed 32 kilograms (71 lb), had a diameter of 75 millimetres (3.0 in) and flew 15 times between November 1967 and September 1968. The RH-100

1517-655: Was the M-100. Some 6640 M-100 sounding rockets were flown from 1957 to 1990. Other early users of Sounding Rockets were Britain, France and Japan. Great Britain developed the Skylark (rocket) series and the later Skua for the International Geophysical Year . France had begun the design of a Super V-2 but that program had been abandoned in the late 1940s due to the inability of France to manufacture all components necessary. Though development of

1558-455: Was the first rocket launched by India from the TERLS ( Thumba Equatorial Rocket Launching Station ) of Kerala in November 1963. The Nike-Apache configuration was also used by one variation of the U.S. Army's MQR-13 BMTS target rocket. [REDACTED] Media related to Nike Apache at Wikimedia Commons Sounding rocket A sounding rocket or rocketsonde , sometimes called

1599-541: Was the last nation to launch a new liquid fueled sounding rocket, the T-7. It was first fired from a very primitive launch site, where the "command center" and borrowed power generator were in a grass hut separated from the launcher by a small river. There was no communications equipment- not even a telephone between the command post and the rocket launcher. The T-7 led to the T-7M, T-7A, T-7A-S, T-7A-S2 and T-7/GF-01A. The T-7/ GF-01A

1640-772: Was used in 1969 to launch the FSW satellite technology development missions. Thus the I-7 led to the first Chinese satellite, the Dong Fang Hong 1 (The East is Red 1), launched by a DF-1. Vital to the development of Chinese rocketry and the Dong Feng-1 was Qian Xuesen (Tsien Hsue-shen in Wade Guiles transliteration) who with Theodore von Kármán and the California Institute of Technology "Suicide Squad" created

1681-411: Was used in testing and perfecting various techniques like staging, destruct system, separation devices and clustering. It was also used as a booster to the weather forecasting rockets. As such it was named as Menaka II which worked along with Menaka I. The RH-200 is a two-stage rocket that can reach up to a maximum altitude of 80 kilometres (50 mi). Solid motors power the first and second stages of

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