Stasiun Peluncuran Roket
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Stasiun Peluncuran Roket
Stasiun Peluncuran Roket or Staspro (literally "Rocket Launching Station") is a rocket launch site managed by the Indonesian National Institute of Aeronautics and Space (LAPAN). It is located at Pameungpeuk Beach in the Garut Regency on West Java near Cilautereun and has been active since 1965 to perform engine tests and launch sounding rockets. The facility was built from 1963 through cooperation between Indonesia and Japan, as the station was designed by Hideo Itokawa with the aim to support high-atmospheric research using Kappa-8 rockets. The first Kappa launch from Pameungpeuk took place on 7 August 1965. Today the site comprises a Motor Assembly building, a Launch Control Center, a Meteorological Sounding System building, a Rocket Motor Storage hangar and a dormitory. The site has launched numerous solid-fuel rockets from the RX family (''Roket Eksperimental''), in particular the RX-250-LPN. Newer developments focus on building multi-stage rockets from individual RX ele ...
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Pameungpeuk
Pameungpeuk is a small town near the coast of southwestern Java, Indonesia. It is located 131 kilometres by road south of Bandung. Geography The town is located several kilometres to the southeast of the small settlement of Cikelet, although it is Cikelet which is the administrative centre of the Cikelet District of the Garut Regency which Pameungpeuk is administered by. The smaller settlements of Mancagahar lie to the southwest, Mandalakasih to the east and Paas along the road to the north. The Kaso River flows past the village into the sea. A picturesque, twisting road is said to lead south from Garut with vegetable plots and tea plantations in the area. A bus service runs along this road from Garut. The road also connects the town to the Papandajan volcano. Pameungpeuk Bay and the white sandy beaches in the coastal area are described as "beautiful" and "stunning". History It contains the Puskesmas Puskesmas ( id, Pusat Kesehatan Masyarakat, ) are government-mandated ...
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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; they were used in warfare by the Arabs, Chinese, Persians, Mongols, and Indians as early as the 13th century. All rockets used some form of solid or powdered propellant up until the 20th century, when liquid-propellant rockets offered more efficient and controllable alternatives. Solid rockets are still used today in military armaments worldwide, model rockets, solid rocket boosters and on larger applications for their simplicity and reliability. Since solid-fuel rockets can remain in storage for an extended period without much propellant degradation and because 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 mode ...
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Rocket Launch Sites
This article constitutes a list of rocket launch sites. Some of these sites are known as spaceports or cosmodromes. A single rocket launch is sufficient for inclusion in the table, as long as the site is properly documented through a reference. Missile locations with no launches are not included in the list. Proposed and planned sites and sites under construction are not included in the main tabulation, but may appear in condensed lists under the tables. A shorter list of spaceports for human spaceflight and satellite launches is available in the article Spaceport. Table specification Sorting order * Countries in alphabetical order within a table * Launch sites within a country are sorted chronologically according to start of operations Column specification * Country – territory of the site (the organisation responsible for the launches may reside elsewhere, as indicated in the notes column; * Location – Name of launch site (sometimes also province etc.) * Coordinates – ge ...
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Encyclopedia Astronautica
The ''Encyclopedia Astronautica'' is a reference web site on space travel. A comprehensive catalog of vehicles, technology, astronauts, and flights, it includes information from most countries that have had an active rocket research program, from Robert Goddard to the NASA Space Shuttle and the Soviet Buran programme. Founded in 1994 and maintained for most of its existence by space enthusiast and author Mark Wade. He has been collecting such information for most of his life. Between 1996 and 2000 the site was hosted by ''Friends and Partners in Space''. The site is no longer updated or maintained and is now considered as partially unreliable. Although it contains a great deal of information, not all of it is correct. Reception and accolades The American Astronautical Society gave the site the Ordway Award for Sustained Excellence in Spaceflight History which "recognizes exceptional, sustained efforts to inform and educate on spaceflight and its history through one or more med ...
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Range Safety
In the field of rocketry, range safety may be assured by a system which is intended to protect people and assets on both the rocket range and downrange in cases when a launch vehicle might endanger them. For a rocket deemed to be ''off course'', range safety may be implemented by something as simple as commanding the rocket to shut down the propulsion system or by something as sophisticated as an independent ''Flight Termination System'' (FTS), which has redundant transceivers in the launch vehicle that can receive a command to self-destruct then set off charges in the launch vehicle to combust the rocket propellants at altitude. Not all national space programs use flight termination systems on launch vehicles. Range safety officers or RSOs are also present in the hobby of model rocketry and then are usually responsible for ensuring a rocket is built correctly, using a safe engine/recovery device, and launched correctly. Flight termination Ground controlled termination Some la ...
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Office Of Commercial Space Transportation
The Office of Commercial Space Transportation (generally referred to as FAA/AST or simply AST) is the branch of the United States Federal Aviation Administration (FAA) that approves any commercial rocket launch operations — that is, any launches that are not classified as model, amateur, or "by and for the government" — in the case of a U.S. launch operator and/or a launch from the U.S. History With the signing of Executive Order 12465 on February 25, 1984, President Reagan designated the Department of Transportation to be the lead agency for commercial expendable launch vehicles. This selection occurred following an interagency competition between the Departments of Commerce and Transportation to be the lead agency. At the time, Congress and the industry supported the Department of Commerce for the lead role, and draft legislation named the Department of Commerce as the agency responsible for the new industry. However, it was the Administration's call, and, moreover, ...
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Launch Pad
A launch pad is an above-ground facility from which a rocket-powered missile or space vehicle is vertically launched. The term ''launch pad'' can be used to describe just the central launch platform (mobile launcher platform), or the entire complex (launch complex). The entire complex will include a ''launch mount'' or ''launch platform'' to physically support the vehicle, a service structure with umbilicals, and the infrastructure required to provide propellants, cryogenic fluids, electrical power, communications, telemetry, rocket assembly, payload processing, storage facilities for propellants and gases, equipment, access roads, and drainage. Most launch pads include fixed service structures to provide one or more access platforms to assemble, inspect, and maintain the vehicle and to allow access to the spacecraft, including the loading of crew. The pad may contain a flame deflection structure to prevent the intense heat of the rocket exhaust from damaging the vehicle or p ...
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List Of Human Spaceflights
This is a list of all human spaceflights throughout history. Beginning in 1961 with the flight of Yuri Gagarin aboard Vostok 1, human spaceflight occurs when a human crew flies a spacecraft into outer space. Human spaceflight is distinguished from spaceflight generally, which entails both crewed and uncrewed spacecraft. There are two definitions of spaceflight. The Fédération Aéronautique Internationale (FAI), an international record-keeping body, defines the boundary between Earth's atmosphere and outer space at above sea level. This boundary is known as the Kármán line. Additionally, the United States awards astronaut wings to qualified personnel who pilot a spaceflight above an altitude of . As of the launch of Shenzhou 15 on 29 November 2022, there have been 367 human spaceflight launches. Two missions did not cross either the Kármán line or the U.S. definition of space and therefore do not qualify as spaceflights. These were the fatal STS-51-L (Challenger disas ...
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Orbital Spaceflight
An orbital spaceflight (or orbital flight) is a spaceflight in which a spacecraft is placed on a trajectory where it could remain in space for at least one orbit. To do this around the Earth, it must be on a free trajectory which has an altitude at perigee (altitude at closest approach) around ; this is the boundary of space as defined by NASA, the US Air Force and the FAA. To remain in orbit at this altitude requires an orbital speed of ~7.8 km/s. Orbital speed is slower for higher orbits, but attaining them requires greater delta-v. The Fédération Aéronautique Internationale has established the Kármán line at an altitude of as a working definition for the boundary between aeronautics and astronautics. This is used because at an altitude of about , as Theodore von Kármán calculated, a vehicle would have to travel faster than orbital velocity to derive sufficient aerodynamic lift from the atmosphere to support itself. Due to atmospheric drag, the lowest altitude ...
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Roket Pengorbit Satelit
The RX rocket family (''Roket Eksperimental'', en, Experimental Rocket) is a series of solid-fuel rockets developed by the Indonesian National Institute of Aeronautics and Space (LAPAN). They are simply named by their diameter in millimeters; for example, the RX-250 has a diameter of . Individual boosters This family is composed of: RX-250 was launched eight times from 1987 to 2007. RX-320 was launched twice in 2008 and once again in 2014. RX-420 flew just once in 2009; it is superseded by RX-450 which was launched on 13 May 2015 , the next booster version RX-550 is under construction; the larger ones are only on the drawing board. Multi-stage rockets Once the solid boosters are fully qualified, LAPAN plans to assemble several of them into multi-stage rockets called ''Roket Pengorbit Satelit'' or ''RPS''. Four staging configurations have been retained so far: * RPS-01 Variant 1 (ex-RPS-420) :* First stage: 3 x RX-420 :* Second stage: 1 x RX-420 :* Third stage: 1 x RX-420 (s ...
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Multi-stage Rocket
A multistage rocket or step rocket is a launch vehicle that uses two or more rocket ''stages'', each of which contains its own engines and propellant. A ''tandem'' or ''serial'' stage is mounted on top of another stage; a ''parallel'' stage is attached alongside another stage. The result is effectively two or more rockets stacked on top of or attached next to each other. Two-stage rockets are quite common, but rockets with as many as five separate stages have been successfully launched. By jettisoning stages when they run out of propellant, the mass of the remaining rocket is decreased. Each successive stage can also be optimized for its specific operating conditions, such as decreased atmospheric pressure at higher altitudes. This ''staging'' allows the thrust of the remaining stages to more easily accelerate the rocket to its final speed and height. In serial or tandem staging schemes, the first stage is at the bottom and is usually the largest, the second stage and subsequ ...
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RX-250-LPN
The RX-250-LPN is an Indonesian sounding rocket, part of the RX rocket family. It was launched six times between 1987 and 2007. Technical data Specifications come from the rocket's summary datasheet published by Indonesian space agency LAPAN. *Apogee: 70 kilometres *Liftoff thrust: 53 kilonewtons *Burning time: 6 seconds *Specific impulse: 220 seconds *Propellant: HTPB *Total mass: 300 kilograms *Core diameter: 0.25 metre The metre (British spelling) or meter (American spelling; see spelling differences) (from the French unit , from the Greek noun , "measure"), symbol m, is the primary unit of length in the International System of Units (SI), though its pref ...s *Total length: 5.30 metres *Payload: 30–60 kg References Rockets and missiles Space launch vehicles of Indonesia {{Indonesia-stub ...
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