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M-V rocket

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M-V rocket
NameM-V rocket
CountryJapan
ManufacturerNissan Motor Co., Ltd. and ISAS
Height30.8 m
Diameter2.5 m
Mass139,000 kg
Payload1,800 kg

M-V rocket is a Japanese launch vehicle developed by the Institute of Space and Astronautical Science (ISAS) and Nissan Motor Co., Ltd.. The M-V rocket was designed to launch scientific satellites and spacecraft into low Earth orbit and beyond, with its first launch taking place on February 10, 2000, from the Uchinoura Space Center in Kyushu, Japan. The M-V rocket played a crucial role in the launch of several notable spacecraft, including the Hayabusa asteroid space probe and the Suzaku X-ray observatory. The development of the M-V rocket involved collaboration with various organizations, including the Japanese Ministry of Education, Culture, Sports, Science and Technology and the Japan Aerospace Exploration Agency (JAXA).

Introduction

The M-V rocket was a significant development in the field of space exploration in Japan, with its design and capabilities allowing for the launch of a range of spacecraft and satellites. The M-V rocket was also used to launch interplanetary spacecraft, such as the Nozomi Mars space probe, which was launched on July 4, 1998, from the Kagoshima Space Center in Kyushu, Japan. The M-V rocket's development was influenced by the work of notable space agencies, including the National Aeronautics and Space Administration (NASA) and the European Space Agency (ESA). The M-V rocket's launch history is closely tied to the work of ISAS and other Japanese space agencies, including the National Space Development Agency of Japan (NASDA) and the Japan Science and Technology Agency (JST).

Design and Development

The M-V rocket was designed and developed by a team of engineers and scientists from ISAS and Nissan Motor Co., Ltd., with input from other organizations, including the University of Tokyo and the Tokyo Institute of Technology. The M-V rocket's design was influenced by the work of notable engineers, including Qian Xuesen and Sergei Korolev, who played a significant role in the development of rocket technology in the Soviet Union and China. The M-V rocket's development involved the use of advanced materials and technologies, including composite materials and cryogenic fuels, which were also used in the development of other launch vehicles, such as the Ariane 5 and the Delta IV. The M-V rocket's design and development were also influenced by the work of notable space agencies, including the Canadian Space Agency (CSA) and the Indian Space Research Organisation (ISRO).

Operational History

The M-V rocket had a relatively short operational history, with its first launch taking place on February 10, 2000, and its final launch on September 22, 2006. During its operational history, the M-V rocket was used to launch a range of spacecraft and satellites, including the Hayabusa asteroid space probe and the Suzaku X-ray observatory. The M-V rocket's operational history was marked by several notable events, including the launch of the Nozomi Mars space probe and the Akari infrared astronomy satellite. The M-V rocket's operational history was also influenced by the work of notable space agencies, including the European Space Agency (ESA) and the Chinese National Space Administration (CNSA). The M-V rocket's launch history is closely tied to the work of ISAS and other Japanese space agencies, including the Japan Aerospace Exploration Agency (JAXA) and the National Space Development Agency of Japan (NASDA).

Specifications

The M-V rocket had a range of specifications, including a height of 30.8 meters and a diameter of 2.5 meters. The M-V rocket had a mass of 139,000 kilograms and was capable of carrying a payload of up to 1,800 kilograms into low Earth orbit. The M-V rocket was powered by a range of engines, including the M-14 and the M-24, which were developed by Nissan Motor Co., Ltd. and ISAS. The M-V rocket's specifications were influenced by the work of notable engineers, including Wernher von Braun and Sergei Korolev, who played a significant role in the development of rocket technology in the United States and the Soviet Union. The M-V rocket's specifications were also influenced by the work of notable space agencies, including the National Aeronautics and Space Administration (NASA) and the Canadian Space Agency (CSA).

Launch History

The M-V rocket had a total of seven launches during its operational history, with its first launch taking place on February 10, 2000, and its final launch on September 22, 2006. The M-V rocket's launch history includes the launch of several notable spacecraft, including the Hayabusa asteroid space probe and the Suzaku X-ray observatory. The M-V rocket's launch history is closely tied to the work of ISAS and other Japanese space agencies, including the Japan Aerospace Exploration Agency (JAXA) and the National Space Development Agency of Japan (NASDA). The M-V rocket's launch history was also influenced by the work of notable space agencies, including the European Space Agency (ESA) and the Indian Space Research Organisation (ISRO). The M-V rocket's launch history includes launches from the Uchinoura Space Center in Kyushu, Japan, and the Kagoshima Space Center in Kyushu, Japan.

Category:Spaceflight