STSAT-2B

Last updated
STSAT-2B
Mission typeTechnology
Operator KARI
Mission duration2 years (planned) [1]
Failed to orbit
Spacecraft properties
Launch mass100 kilograms (220 lb) [2]
Start of mission
Launch date10 June 2010, 08:01 (2010-06-10UTC08:01Z) UTC [3]
Rocket Naro-1
Launch site Naro
Contractor Khrunichev/KARI
Orbital parameters
Reference system Geocentric
Regime Low Earth (planned)
Failed to orbit
Perigee altitude 300 kilometres (190 mi) [2]
Apogee altitude 1,500 kilometres (930 mi) [2]
Inclination 80 degrees [2]
Epoch Planned
 

STSAT-2B, or Science and Technology Satellite 2B, was a South Korean satellite which was lost in the failure of the second flight of the Naro-1 carrier rocket. It was to have been operated by the Korea Aerospace Research Institute, and was intended to demonstrate technology for future spacecraft. The satellite had a mass of 100 kilograms (220 lb), [2] and was expected to operate for at least two years. [1]

South Korea Republic in East Asia

South Korea is a country in East Asia, constituting the southern part of the Korean Peninsula and sharing a land border with North Korea. The name Korea is derived from Goguryeo which was one of the great powers in East Asia during its time, ruling most of the Korean Peninsula, Manchuria, parts of the Russian Far East and Inner Mongolia under Gwanggaeto the Great. Its capital, Seoul, is a major global city and half of South Korea's over 51 million people live in the Seoul Capital Area, the fourth largest metropolitan economy in the world.

Satellite Human-made object put into an orbit

In the context of spaceflight, a satellite is an object that has been intentionally placed into orbit. These objects are called artificial satellites to distinguish them from natural satellites such as Earth's Moon.

Naro-1 South Korean carrier rocket

Naro-1, previously designated the Korea Space Launch Vehicle or KSLV, is South Korea's first carrier rocket, and the first South Korean launch vehicle to achieve Earth orbit. On 30 January 2013 the third Naro-1 vehicle built successfully placed STSAT-2C into low Earth orbit.

Contents

STSAT-2B was originally intended to operate alongside a second spacecraft, STSAT-2A; however STSAT-2A was lost in 2009 after the payload fairing of its carrier rocket failed to separate, leaving the rocket unable to achieve orbit. [4]

STSAT-2A was a satellite launched by the Korea Aerospace Research Institute (KARI), the national space agency of South Korea, from the Naro Space Center in Goheung County, South Jeolla using the Naro-1 (KSLV-1) rocket.

Instruments

The primary instrument aboard STSAT-2B was the Dual-channel Radiometer for Earth and Atmosphere Monitoring, or DREAM, which would have measured the brightness temperature of the Earth at 23.8 GHz and 37 GHz. [5] The secondary payload, the Laser Retroreflector Array or LRA was to have been used for the Satellite Laser Ranging experiment, which was intended to determine the parameters of the satellite's orbit with a greater degree of precision. Data collected by the secondary payload would have been used to calibrate DREAM, to conduct geodetic research, and to evaluate the performance of the carrier rocket. [1] Due to lower manufacturing tolerance, the retroreflectors on STSAT-2B would have provided greater precision than those intended on STSAT-2A. [6]

Brightness temperature or radiance temperature is the temperature of a black body in thermal equilibrium with its surroundings, in order to duplicate the observed intensity of a grey body object at a frequency . This concept is used in radio astronomy, planetary science and materials science.

Geodesy The science of the geometric shape, orientation in space, and gravitational field of Earth

Geodesy is the Earth science of accurately measuring and understanding Earth's geometric shape, orientation in space and gravitational field. The field also incorporates studies of how these properties change over time and equivalent measurements for other planets. Geodynamical phenomena include crustal motion, tides and polar motion, which can be studied by designing global and national control networks, applying space and terrestrial techniques and relying on datums and coordinate systems.

A series of technological experiments were also to have been conducted; investigating attitude control systems, and testing pulsed plasma thrusters, star trackers, a Sun sensor, as well as an experimental onboard computer, and data relay at rates of up to 10 megabits per second. [1]

Attitude control is controlling the orientation of an object with respect to an inertial frame of reference or another entity like the celestial sphere, certain fields, and nearby objects, etc.

A pulsed plasma thruster (PPT), also known as a plasma jet engine, is a form of electric spacecraft propulsion. PPTs are generally considered the simplest form of electric spacecraft propulsion and were the first form of electric propulsion to be flown in space, having flown on two Soviet probes starting in 1964. PPTs are generally flown on spacecraft with a surplus of electricity from abundantly available solar energy.

Star tracker device that senses the direction to one or multiple stars

A star tracker is an optical device that measures the positions of stars using photocells or a camera. As the positions of many stars have been measured by astronomers to a high degree of accuracy, a star tracker on a satellite or spacecraft may be used to determine the orientation of the spacecraft with respect to the stars. In order to do this, the star tracker must obtain an image of the stars, measure their apparent position in the reference frame of the spacecraft, and identify the stars so their position can be compared with their known absolute position from a star catalog. A star tracker may include a processor to identify stars by comparing the pattern of observed stars with the known pattern of stars in the sky.

Launch

STSAT-2B was launched by a Naro-1 rocket, flying from the Naro Space Centre. The launch was the second flight of the Naro-1, which consisted of a modified Angara first stage manufactured by Khrunichev, [7] and a South Korean solid-fuelled upper stage. The previous Naro-1 launch was that of STSAT-2A, which occurred in August 2009 and ended in failure. [4]

Naro Space Center is a South Korean spaceport in South Jeolla's Goheung County, operated by the state-run Korea Aerospace Research Institute.

Angara (rocket family) family of space-launch vehicles

The Angara rocket family is a family of space-launch vehicles being developed by the Moscow-based Khrunichev State Research and Production Space Center. The rockets are to put between 3,800 and 24,500 kg into low Earth orbit and are intended, along with Soyuz-2 variants, to replace several existing launch vehicles.

Khrunichev State Research and Production Space Center Moscow-based producer of spacecraft and space-launch systems

The Khrunichev State Research and Production Space Center is a Moscow-based manufacturer of spacecraft and space-launch systems, including the Proton and Rokot rockets, and the Russian modules of Mir and the International Space Station.

The launch was initially scheduled to occur on 9 June 2010, during a two-hour launch window opening at 07:30 UTC (16:30 local time). Further launch attempts were available at the same time each day until 19 June 2010. [8] The launch attempt on 9 June 2010 was scrubbed after the launch pad's fire suppression system activated for no apparent reason.

Launch window time period during which a space vehicle must be launched in order to reach its intended target

In the context of spaceflight, launch period is the collection of days and launch window is the time period on a given day during which a particular vehicle must be launched in order to reach its intended target. If the rocket is not launched within a given window, it has to wait for the window on the next day of the period. Launch periods and launch windows are very dependent on both the rocket's capability and the orbit to which it is going.

Following the scrub, the launch was rescheduled for the next day, and took place at 08:01 UTC (17:01 local time) on 10 June 2010. [3] During the first stage burn, around 137 seconds into the flight, contact with the rocket was lost. [9] South Korean science minister Ahn Byung-man later told reporters that the rocket was believed to have exploded. [10] If the launch had been successful, STSAT-2B would have been deployed into an orbit with a perigee of approximately 300 kilometres (190 mi), an apogee of approximately 1,500 kilometres (930 mi), and around 80 degrees of inclination. [2]

Flight termination system malfunction

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Orbital Sciences Corporation was an American company specializing in the design, manufacture and launch of small- and medium- class space and rocket systems for commercial, military and other government customers. In 2014 Orbital merged with Alliant Techsystems to create a new company called Orbital ATK, Inc., which in turn was purchased by Northrop Grumman in 2018. Orbital Sciences Corporation today is a subsidiary of Northrop Grumman and is known as Northrop Grumman Innovation Systems.

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Korea Aerospace Research Institute

The Korea Aerospace Research Institute (KARI) established in 1989, is the aeronautics and space agency of South Korea. Its main laboratories are located in Daejeon, in the Daedeok Science Town. KARI's vision is to continue building upon indigenous launch capabilities, strengthen national safety and public service, industrialize satellite information and applications technology, explore the moon, and develop environmentally-friendly and highly-efficient cutting-edge aircraft and core aerospace technology. Current projects include the KSLV-2 launcher. Past projects include the 1999 Arirang-1 satellite. The agency was founded in 1989. Prior to South Korea's entry into the IAE in 1992, it focused primarily on aerospace technology.

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STSAT-2C

STSAT-2C, or Science and Technology Satellite 2C, or Naro Science Satellite(ko:나로과학위성) is a South Korean satellite which was launched in 2013. It is operated by the Korea Aerospace Research Institute, and is intended to demonstrate technology for future spacecraft. The satellite has a mass of 100 kilograms (220 lb), and is expected to operate for less than a year.

Science and technology in South Korea has advanced throughout the decades.

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References

  1. 1 2 3 4 Noll, Carey. "ILRS Mission Support Status". STSAT-2 Satellite Information. NASA. Archived from the original on 25 May 2010. Retrieved 24 April 2010.
  2. 1 2 3 4 5 6 Noll, Carey. "STSAT-2". STSAT-2 Satellite Information. NASA. Archived from the original on 16 May 2010. Retrieved 24 April 2010.
  3. 1 2 "(rocket launch) S. Korea's Naro-1 rocket lifts off from space center". Yonhap News. 10 June 2010. Retrieved 10 June 2010.
  4. 1 2 Lee Joon-seung (26 August 2010). "S. Korean satellite lost shortly after launch: gov't". Yonhap News Agency. Retrieved 24 April 2010.
  5. Dual-channel radiometers for Earth and atmosphere monitoring (DREAM) on micro satellite STSAT-2
  6. Noll, Carey. "RetroReflector Array (RRA) Characteristics". STSAT-2 Satellite Information. NASA. Archived from the original on 24 May 2010. Retrieved 24 April 2010.
  7. "First-Stage Engine of Naro-1 to Arrive on Weekend". Arirang. 2 April 2010. Retrieved 24 April 2010.
  8. Jang Ji-yun (20 April 2010). "Korea to Launch 2nd Naro Space Rocket on June 9". Arirang. Retrieved 24 April 2010.
  9. "(LEAD) (rocket launch) Ground controllers lose contact with space rocket after takeoff". Yonhap News. 10 June 2010. Retrieved 10 June 2010.
  10. "S Korean space rocket might have exploded: science minister". Xinhua. 10 June 2010. Archived from the original on 12 June 2010. Retrieved 10 June 2010.