
Naroho
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KSLV-Ⅰ Naro KSLV-Ⅰ "Naro" | |
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designation | Korean Launch Vehicle-I (Korea Space Launch Vehicle-Ⅰ) to me (Naro) |
development plan | |
Usage | low earth orbit satellite launch |
producer | |
country of use | |
situation | retired |
specifications | |
Battlefield | 33.5 m |
Stage 1 : 25.8 m | 2nd stage : 7.7 m | |
diameter | 2.9 m |
weight | 140 t |
singular | 2nd stage |
payload capacity | 100 kg (300km LEO) |
single stage rocket | |
engine | |
thrust | 170 t (sea surface) , 180 t (vacuum) |
Specific impulse (SI) | 311 s (sea surface) , 337 s (vacuum) |
burning time | 230 s |
propellant | Liquid Propellant (RP-1/Liquid Oxygen) |
2 stage rocket | |
engine | 1 × KM ( South Korea ) |
thrust | 8 t |
Specific impulse (SI) | 288 s |
burning time | 60 s |
propellant | solid propellant |
launch record | |
launch site | Naro Space Center 1st launch pad |
total number of shots | 3 (Success: 1 / Failure: 2) |
launch date | |
1. outline
The Naro-ho or KSLV-I (Korea Space Launch Vehicle-I) was developed by the Korea Aerospace Research Institute in 2002 according to the KSLV plan , and was developed three times in 2009 , 2010 , and 2013 . It is Korea's first space launch rocket . About KRW 500 billion was invested in the development , and the first stage rocket used the RD-151 engine developed by Energomarsh of Russia , and the second stage rocket used an 8-ton solid rocket manufactured by itself. The first and second launches failed due to unseparated fairings and air explosions, respectively, and the third launch succeeded in putting the Naro Science Satellite (STSAT-2C) into low earth orbit.
After the success of KSLV-I, Korea Aerospace Research Institute has been carrying out a plan for a rocket (KSLV-II) for launching low-orbit practical satellites with a domestically produced first-stage rocket, and as a result, in 2021 Nuriho was developed.
The name 'Naro' was selected through a national naming contest and was the first space center in Korea where a rocket was launched. The name of the Naro Space Center and Jeollanam- do, where the space center is located Goheung-gun It is derived from Oenarodo .[1] It is said that the name Narodo comes from the fact that the island looks like windblown silk when viewed from the sea . #
After the success of KSLV-I, Korea Aerospace Research Institute has been carrying out a plan for a rocket (KSLV-II) for launching low-orbit practical satellites with a domestically produced first-stage rocket, and as a result, in 2021 Nuriho was developed.
The name 'Naro' was selected through a national naming contest and was the first space center in Korea where a rocket was launched. The name of the Naro Space Center and Jeollanam- do, where the space center is located Goheung-gun It is derived from Oenarodo .[1] It is said that the name Narodo comes from the fact that the island looks like windblown silk when viewed from the sea . #
2. history
3. specifications
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specifications | ||
singular | 2nd stage[2] | |
height | 33.5 m | |
diameter | 2.9 m | |
gross weight[3] | 140 t | |
dry weight | 10 t | |
fuel load | 130 t | |
fuel/oxidizer | Kerosene (RP-1) / Liquid Oxygen | |
payload | 100 kg (300km LEO) | |
thrust | 213,600 kgf | |
engine | 1 stage | |
2nd stage | Kick Motor[4] (thrust: 9.6 t) | |
For reference, the thickness of the fuel tank is only 2 mm , and since such a tank cannot withstand its own weight or is easily damaged when empty, it is filled with helium during transportation. This tank structure has long been used to reduce the weight of rockets.[5] It is one of the commonly used methods and can collapse or collapse if it fails to maintain internal pressure.[6]
4. mounted satellite
Initially, the name of the satellite created to launch KSLV-I was Science and Technology Satellite No. 2 . To be precise, two identical satellites were created to launch the first and second launches of the Naro, and were numbered STSAT-2A and STSAT-2B, respectively. The problem was initially made to prepare for the launch in 2005 according to the plan, but as the launch continued to be delayed, it went to storage for over four years. In this way, both the first and second launches, which were barely performed, failed, and both satellites could not reach orbit and were consumed.
Therefore, the newly manufactured Naro Science Satellite (STSAT-2C) for the third launch was smaller and had more simplified functions than before for reasons such as time and budget. It orbits the Earth once every 103 minutes and performs missions such as measuring space radiation, observing the space ionosphere, and verifying domestically developed space technology. Since the main mission is to confirm satellite entry into orbit and check satellite status, the expected lifespan was short at one year. It is said that it has been active for about 3 months longer than its expected lifespan and has been no longer in communication since April 2014. #
Therefore, the newly manufactured Naro Science Satellite (STSAT-2C) for the third launch was smaller and had more simplified functions than before for reasons such as time and budget. It orbits the Earth once every 103 minutes and performs missions such as measuring space radiation, observing the space ionosphere, and verifying domestically developed space technology. Since the main mission is to confirm satellite entry into orbit and check satellite status, the expected lifespan was short at one year. It is said that it has been active for about 3 months longer than its expected lifespan and has been no longer in communication since April 2014. #
5. evaluation
5.1. result

"Through the development of the Naro, the level of domestic launch vehicle technology has improved from 46.3% to 83.4% compared to developed countries"Korean launch vehicle detailed planning study, analysis of domestic technology level improvement (National Research Foundation, '09.5)
It is not an exaggeration to say that prior to the development of the Naro, Korea's space launch vehicle-related technology was at the level of a blank sheet of paper that fell short of the rudimentary level. Under such circumstances, he acquired numerous technologies directly or indirectly through cooperation with Russia. Overall, there has been tremendous technological progress, and it is judged that this will be of great help to the future development of the Korean launch vehicle .
Among them, the most prominent technologies are launch vehicle system technology and launch site ground system technology. All systems, not just space launch vehicles, are more than just the sum of their parts. From the initial design stage, it is necessary to decide what form and function to have, what parts to use for this purpose, what are the requirements for such parts, etc. It is necessary to test and verify how to assemble the parts systematically and whether the parts are gathered together and operate smoothly, etc. Even after that, how to operate the assembled system, how to establish the procedure for launching it, and overseeing the entire work A number of systematic developments, such as how to configure control techniques, are required. These technologies cannot be obtained in the form of documents or products, and can only be learned through direct implementation. Korea, along with Russia, which has world-class technology and experience, develops the development process from design → manufacturing → testing → assembly → launch operation → launch. It was learned as it was while working together.
According to the Korea-Russia task division, Russia was in charge of Tier 1 and Korea was responsible for Tier 2, but as the entire system development process was jointly conducted by Korea and Russia, the content of the task division is detailed. Simply dividing the Naro into 1st stage + 2nd stage, 1st stage is a Russian rocket and 2nd stage is a Korean rocket.
Also, a fact that is not well known, the development of a 30-ton liquid rocket engine developed by Hangwoon on its own was also carried out with the Naroho budget. This is because it was originally developed in preparation for the case where KSLV-I development was changed to independent development in the middle.[7] The development of this 30-ton class engine is the Nuri-ho 75-ton class engine . Therefore, it is said that the design similarity between the 30-ton engine and the 75-ton engine is high. Analytical Consideration of Combustor Design of Korean Launch Vehicle Liquid Rocket Engine
In addition, the Naro's two-stage kick motor design will be used as the first-stage propellant of a Korean hypersonic missile .
Among them, the most prominent technologies are launch vehicle system technology and launch site ground system technology. All systems, not just space launch vehicles, are more than just the sum of their parts. From the initial design stage, it is necessary to decide what form and function to have, what parts to use for this purpose, what are the requirements for such parts, etc. It is necessary to test and verify how to assemble the parts systematically and whether the parts are gathered together and operate smoothly, etc. Even after that, how to operate the assembled system, how to establish the procedure for launching it, and overseeing the entire work A number of systematic developments, such as how to configure control techniques, are required. These technologies cannot be obtained in the form of documents or products, and can only be learned through direct implementation. Korea, along with Russia, which has world-class technology and experience, develops the development process from design → manufacturing → testing → assembly → launch operation → launch. It was learned as it was while working together.
According to the Korea-Russia task division, Russia was in charge of Tier 1 and Korea was responsible for Tier 2, but as the entire system development process was jointly conducted by Korea and Russia, the content of the task division is detailed. Simply dividing the Naro into 1st stage + 2nd stage, 1st stage is a Russian rocket and 2nd stage is a Korean rocket.
Also, a fact that is not well known, the development of a 30-ton liquid rocket engine developed by Hangwoon on its own was also carried out with the Naroho budget. This is because it was originally developed in preparation for the case where KSLV-I development was changed to independent development in the middle.[7] The development of this 30-ton class engine is the Nuri-ho 75-ton class engine . Therefore, it is said that the design similarity between the 30-ton engine and the 75-ton engine is high. Analytical Consideration of Combustor Design of Korean Launch Vehicle Liquid Rocket Engine
In addition, the Naro's two-stage kick motor design will be used as the first-stage propellant of a Korean hypersonic missile .
5.2. Limit
The fact that the plan was delayed several times during the development process can be seen as a point that should be criticized. It is said that the schedule has been constantly disrupted due to the complex international cooperation system in which Korea Aerospace Research Institute, the Russian government, and three space companies are intertwined. In fact, even if unavoidable cases such as disruptions in parts supply due to the Sichuan earthquake or interruption due to problems during launch attempts were excluded, the agreement was signed and ratified, test items were added, test schedule issues, data analysis issues, etc. until the first launch attempt. This has only been postponed 5 times.
Thanks to this, he succeeded in entering the orbit of a space launch vehicle later than North Korea 's Eunha 3, and was criticized for a long time, but he managed to save face by succeeding in the 3rd launch of Naro anyway.
Thanks to this, he succeeded in entering the orbit of a space launch vehicle later than North Korea 's Eunha 3, and was criticized for a long time, but he managed to save face by succeeding in the 3rd launch of Naro anyway.
5.2.1. 1st stage engine technology
One of the most famous criticisms of the Naro is the failure to transfer first-stage engine technology. However, in the first place, it was impossible to trade core technologies such as single-stage engine technology within the MTCR system between countries, and both Korea and Russia were aware of this fact from the beginning, so there was no such thing as technology transfer in the initial contract . Criticizing this is like criticizing why you couldn’t receive a technology that was impossible to receive in the first place and had no intention of receiving.
There is also criticism that it is like paying our money and testing the Russian 1st Dan instead, but this is more of a reverse understanding of the context. In fact, joint development was possible because the Russian RD-151 engine used in the first stage was still unfinished. It is also close to impossible to trade finished engines because of MTCR. Considering that the purpose of cooperation with Russia was to acquire projectile system technology through experience through a joint development process, it can be seen as beneficial to both Russia and Korea.
And although this has not been officially revealed, it appears that a significant amount of technology has been acquired indirectly through exchanges between Korean and Russian engineers. The reason why it was not officially revealed is because if this is officially announced, it would be like blatantly certifying that the MTCR was violated (...). If you look at interviews with people involved in development, you can see that in response to criticism that they have not gained anything, they want to say outright that they have learned a lot indirectly, but they seem to be unable to do so, and only give off nuance.[8] The Korean launch vehicle project continued smoothly, and this interpretation gained further support as, in an article in the JoongAng Ilbo on October 29, 2021, Cho Gwang-rae testified that the engine of the ground test launch vehicle, which was known as a model, was in fact the actual RD-151 engine . However, in 2023, after the Russian-Russian War broke out , the Korea Aerospace Research Institute revised and announced that the model rocket it received from Russia was not the original.[9] With this, the official position of the Korea Aerospace Research Institute ended with the fact that the engine itself was a model.
However, since the person who testified that he received the real engine was the director of the Korea Aerospace Research Institute and the person who led the Naro project, this position is completely incoherent. In reality, there was a behind-the-scenes agreement between Russia and South Korea to transfer the original engine and various technologies, but since the confidential information was leaked to the media in the form of a personal interview, it is highly likely that it was just removed at the institutional level.
There is also criticism that it is like paying our money and testing the Russian 1st Dan instead, but this is more of a reverse understanding of the context. In fact, joint development was possible because the Russian RD-151 engine used in the first stage was still unfinished. It is also close to impossible to trade finished engines because of MTCR. Considering that the purpose of cooperation with Russia was to acquire projectile system technology through experience through a joint development process, it can be seen as beneficial to both Russia and Korea.
And although this has not been officially revealed, it appears that a significant amount of technology has been acquired indirectly through exchanges between Korean and Russian engineers. The reason why it was not officially revealed is because if this is officially announced, it would be like blatantly certifying that the MTCR was violated (...). If you look at interviews with people involved in development, you can see that in response to criticism that they have not gained anything, they want to say outright that they have learned a lot indirectly, but they seem to be unable to do so, and only give off nuance.[8] The Korean launch vehicle project continued smoothly, and this interpretation gained further support as, in an article in the JoongAng Ilbo on October 29, 2021, Cho Gwang-rae testified that the engine of the ground test launch vehicle, which was known as a model, was in fact the actual RD-151 engine . However, in 2023, after the Russian-Russian War broke out , the Korea Aerospace Research Institute revised and announced that the model rocket it received from Russia was not the original.[9] With this, the official position of the Korea Aerospace Research Institute ended with the fact that the engine itself was a model.
However, since the person who testified that he received the real engine was the director of the Korea Aerospace Research Institute and the person who led the Naro project, this position is completely incoherent. In reality, there was a behind-the-scenes agreement between Russia and South Korea to transfer the original engine and various technologies, but since the confidential information was leaked to the media in the form of a personal interview, it is highly likely that it was just removed at the institutional level.
5.2.2. Difficulties in development due to external factors
Looking at the change in engine technology used by business since the days of KSR, you can see that it continues to change from solid (KSR-I, II) → liquid (KSR-III) → solid (top of Naro) → liquid (Nuri). , At first glance, it seems that the development of the projectile proceeded without consistency. However, in fact, this problem is due to the geopolitical problems of the Republic of Korea, which have to pay attention to the four major powers.
Solid fuel rockets have the problem that they can be used as intercontinental ballistic missiles as they are.[10] . This issue is a part in which the United States interferes a lot, and the ROK- US missile range guidelines revised in 1990 prohibited the development of any rocket system with a range of 180 km and a warhead weight of 500 kg or more. It was sluggish. This is because there is no option for space development rockets with a range of 180 km. In the end, according to these guidelines, the development of KSR-II, which was a solid, was not allowed to proceed.
In 2001, when the ROK-US missile range guidelines were revised, civilian rockets were changed to those not subject to these guidelines, but in practice, it was not possible to openly make solid fuels. This is because the four major powers surrounding the Korean Peninsula , the United States , China , Japan , and Russia , will not just watch the development of solid fuel rockets that can be used as ballistic missiles. In the end, it was because of these problems that the first stage went to liquid and the second stage went to solid. This problem was practically resolved only in 2020, when the ROK-US missile range guidelines were revised again to allow the use of solid fuel in civilian rockets.[11] Since then , this problem has been completely resolved as the ROK-US missile range guidelines were abolished in 2021.
Solid fuel rockets have the problem that they can be used as intercontinental ballistic missiles as they are.[10] . This issue is a part in which the United States interferes a lot, and the ROK- US missile range guidelines revised in 1990 prohibited the development of any rocket system with a range of 180 km and a warhead weight of 500 kg or more. It was sluggish. This is because there is no option for space development rockets with a range of 180 km. In the end, according to these guidelines, the development of KSR-II, which was a solid, was not allowed to proceed.
In 2001, when the ROK-US missile range guidelines were revised, civilian rockets were changed to those not subject to these guidelines, but in practice, it was not possible to openly make solid fuels. This is because the four major powers surrounding the Korean Peninsula , the United States , China , Japan , and Russia , will not just watch the development of solid fuel rockets that can be used as ballistic missiles. In the end, it was because of these problems that the first stage went to liquid and the second stage went to solid. This problem was practically resolved only in 2020, when the ROK-US missile range guidelines were revised again to allow the use of solid fuel in civilian rockets.[11] Since then , this problem has been completely resolved as the ROK-US missile range guidelines were abolished in 2021.
6. digression
- After the first launch failed, a flash message saying, “ The equipment will be stopped” came out and became popular while going to hit galleries . Then, after the second launch failed, the equipment was stopped. The second flash also went to the hit gallery.
- It was released as a 1/144 model.
- It was successful in the third launch, and as seen above, there were achievements, but as a result, the name 'Naro' on the Internet later became a synonym for a shovel that explodes fiercely or flies away without any results. For example, in the game League of Legends, champions like Jinx and Ashe blow globals. Whenever the ultimate skill flies without hitting anyone, it is called Naro-ho, or in StarCraft 2 , it is said that Na-Ro-Ho falls when the core falls. Or, in soccer, when kicking an absurd aerial ball that cuts through the air, or when a pitcher throws a ball in baseball, it is called Naroho. For example this player .
- Among the Hell Party contents of the online game Dungeon & Fighter , there is an APC called the Cartel Remnants that stole the Naroho . The weapon it drops is the unique epic weapon, the Naro Space.
- There was a commotion in which the kick motor, a core part of the Naro, was sold to a junk dealer and then quickly recovered . The Korea Aerospace Research Institute acknowledged that the key parts were not important because they were left in an outdoor container on the site, and that the handover of the goods was inexperienced. #
- There is an air freshener made by Toystar and licensed by the Korea Aerospace Research Institute .
- After the second launch of the Naro failed, Lee Ju-jin, director of the Korea Aerospace Research Institute , resigned from his post, taking responsibility for the failure .[12] After the successful third launch of the Naro, Cho Kwang-rae , head of the Naro Launch Promotion Team, was appointed as the head of the Korea Aerospace Research Institute .
6.1. Comparison with North Korea
On December 12, 2012, about two weeks after the third Naro launch attempt was suspended and the launch date was delayed, North Korea suddenly succeeded in launching the Unha 3 . Some call it the Korean Peninsula version of Sputnik Shock . It is ironic to think that the KSLV plan was initially set for 2005 as well as the satellite launch date set for 2010 after being shocked by North Korea's launch of Kwangmyongsong-1 in 1999.
However, while the launch vehicle itself was successful, the satellite actually went into orbit but did not operate. It is presumed that the Kwangmyeongseong 3 satellite, which is in orbit, is not performing its satellite function properly because it is circling the orbit while somersaulting in space. # A comparison with the Naro Science Satellite, which successfully communicated after going into orbit .
In addition, in the case of South Korea, since it uses an oxidizing agent rather than red nitric acid for peaceful development, it is relatively more difficult to launch, whereas North Korea uses red nitric acid, which can be fired at any time because it can be stored at room temperature. This means that the purpose of rocket development is different in the first place. Difference between Naro and Eunha 3
Meanwhile, around March 2012, ahead of the launch of Kwangmyeongseong-3, North Korea responded to pressure from South Korea by asking, 'Do those who can't even launch Naro have the right to criticize us?' There was a time when I dissed him by saying, However, the launch of Gwangmyeongseong 3 in April 2012, which was carried out after these words were said, failed.
Ironically, the cause of Naro 1's failure is similar to that of Eunha 2's.[13] The reason for the failure of Naro 2 is similar to that of Eunha 3.[14]
However, while the launch vehicle itself was successful, the satellite actually went into orbit but did not operate. It is presumed that the Kwangmyeongseong 3 satellite, which is in orbit, is not performing its satellite function properly because it is circling the orbit while somersaulting in space. # A comparison with the Naro Science Satellite, which successfully communicated after going into orbit .
In addition, in the case of South Korea, since it uses an oxidizing agent rather than red nitric acid for peaceful development, it is relatively more difficult to launch, whereas North Korea uses red nitric acid, which can be fired at any time because it can be stored at room temperature. This means that the purpose of rocket development is different in the first place. Difference between Naro and Eunha 3
Meanwhile, around March 2012, ahead of the launch of Kwangmyeongseong-3, North Korea responded to pressure from South Korea by asking, 'Do those who can't even launch Naro have the right to criticize us?' There was a time when I dissed him by saying, However, the launch of Gwangmyeongseong 3 in April 2012, which was carried out after these words were said, failed.
Ironically, the cause of Naro 1's failure is similar to that of Eunha 2's.[13] The reason for the failure of Naro 2 is similar to that of Eunha 3.[14]
7. launch record
Naro launch record | |||||
sequential | launch date | launch site | mounted satellite | result | note |
1 | Aug 25, 2009 17:00:33 | Naro Space Center | failure | ||
2 | Jun 10 2010 17:01 | failure | |||
3 | Jan 30, 2013 16:00 | success | |||
7.1. launch process
Naro launch procedure | ||
count down | procedure | note |
T-08:05:00 | start of launch operation | |
T-07:20:00 | Preparation work for first-stage propellant charging begins | |
T-06:58:00 | Overhauled for propellant and helium filling | |
T-06:53:00 | Start of helium charge for valve and engine control | |
T-06:20:00 | 1st stage fuel tank on-board component function work completed | Onboard is the electronic equipment in the launch vehicle. |
T-05:49:00 | 1st stage oxidizer tank on-board component function check completed | |
T-04:31:00 | Start charging the upper posture control system | |
T-04:30:00 | Land introduction begins, withdrawal of technical personnel safety area around the launch pad | |
T-04:12:00 | Completed the withdrawal of technical personnel around the launch pad | |
T-04:00:00 | Ready to charge single stage rocket propellant | |
T-03:56:00 | Start cooling the oxidizer supply system | |
T-02:45:00 | Oxidant supply system cooling completed | |
T-02:43:00 | Start oxidizer tank cooling | |
T-02:13:00 | Oxidant tank cooling complete | |
T-02:02:00 | Start injecting fuel ( kerosene ) into the 1st stage fuel tank of the projectile | |
T-01:56:00 | Projectile 1st stage oxidizer (liquid oxygen) charge start | |
T-01:35:00 | Start filling the helium high-pressure tank | |
T-01:14:00 | Completed injection of fuel (kerosene) into the 1st stage fuel tank of the projectile | |
T-00:54:00 | Projectile 1st stage oxidizer (liquid oxygen) charge complete | |
T-00:50:00 | Withdrawal of the projectile holding device | |
T-00:45:00 | Start of final launch preparation work for upper part and range system | |
T-00:37:00 | Upper part posture control system charging completed | |
T-00:32:00 | Completed withdrawal of projectile erector | |
T-00:18:00 | All systems ready for launch | |
T-00:16:00 | Approval of the final launch of the Naro | |
T-00:15:00 | Final countdown begins (900 seconds) Top battery power supply | |
T-00:00:04 | 1st stage engine ignition | |
T+00:00:00 | launch | 0 seconds after takeoff |
T+00:00:54 | breaking through the speed of sound | 54 seconds after takeoff |
T+00:03:36 | Remove the upper fairing | 216 seconds after takeoff |
T+00:03:50 | 1st stage engine shutdown | 230 seconds after takeoff |
T+00:03:53 | 1st stage rocket separation | 233 seconds after takeoff |
T+00:06:35 | 2nd stage engine ignition | 395 seconds after takeoff |
T+00:07:33 | 2nd stage engine shutdown, target trajectory entry | 445 seconds after takeoff |
T+00:09:00 | satellite separation | 540 seconds after takeoff |
8.
[1] Narodo consists of outer Narodo and inner Narodo.[2] 1st stage liquid propulsion, 2nd stage solid propulsion[3] Launch vehicle dead weight + fuel payload + fairing + payload weight[4] As a solid fuel rocket developed in Korea , it is the first solid rocket launched by burning in space in our history.[5] Even the SM-65 Atlas ICBM does not use an internal frame, and the thin part uses a balloon tank method supported by these tanks, which are only 0.1 inches, so that thickness is not a very unusual factor only for Russia or Naroho. Even now, the fuel tank of the upper stage of the Centaur uses a method of maintaining only the tank without an internal frame.[6] In the past, Atlas-Azena rockets and Ariane rockets used a similar method, but there are cases where they collapsed due to such mistakes in the process of refueling or moving. real video[7] Rumor has it that the test facilities currently testing 75-ton and 7-ton engines were also built with the Naro budget.[8] An interview article by Cho Kwang -rae, former head of the Korea Aerospace Research Institute, who was the head of the Naro launch propulsion team at the time, reveals the tearful efforts of Korean engineers to acquire technology. #[9] Donga Science <The engine provided by Russia is not ‘genuine’… According to “It is not a great help to the development of Korean launch vehicles,” the rumor spread that the development of the Naro engine was successful after looking at an authentic Russian engine, so the researchers’ hard work should not be disparaged.[10] In fact, liquid is also possible, but liquid is difficult to use as a ballistic missile because it takes a lot of preparation time such as fuel injection.[11] This provision is very meaningful because military rockets can be used by slightly improving civilian rockets.[12] There are also rumors that there was pressure from the Ministry of Education, Science and Technology at the time .[13] The Naro 1 is not separated from the fairing, and the Eunha 2 is not separated from the 3rd stage rocket.[14] All explode in the air after 2-3 minutes.[15] Failure to enter satellite orbit due to unseparation of one pairing[16] At that time, the cause of the fairing failure was explained as "the result of using a general wire , not a wire used in a vacuum state." I don't know who uses common wire there #[17] At 137.19 seconds after launch, the first stage rocket exploded and crashed.[18] Since April 2014, communication with the Naro Science Satellite has been cut off, so the satellite operation has virtually ceased.[19] Due to lack of time and budget, the design life itself was shortened to one year. It was launched in January 2013, but the communication was cut off in April 2014, so the Naro Science Satellite has been operating for three months beyond its design lifespan, and then communication is cut off.
- Document deletion movement (KSLV-1 Naro → KSLV-I Naro)
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