
The ETS-VII, or Engineering Test Satellite No. 7, was a
satellite
A satellite or an artificial satellite is an object, typically a spacecraft, placed into orbit around a celestial body. They have a variety of uses, including communication relay, weather forecasting, navigation ( GPS), broadcasting, scient ...
developed and launched by the
National Space Development Agency of Japan (NASDA). It is also known as KIKU-7.
It was launched aboard an
H-II rocket from
Tanegashima Space Center, on 28 November 1997.
The ETS-VII was equipped with a
robotic arm
A robotic arm is a type of mechanical arm, usually programmable, with similar functions to a human arm; the arm may be the sum total of the mechanism or may be part of a more complex robot. The links of such a manipulator are connected by join ...
, which was used to carry out several experiments related to
rendezvous docking and space robotics.
It was the world's first satellite to be equipped with a robotic arm,
and also Japan's first
uncrewed spacecraft
Uncrewed spacecraft or robotic spacecraft are spacecraft without people on board. Uncrewed spacecraft may have varying levels of autonomy from human input, such as remote control, or remote guidance. They may also be autonomous, in which th ...
to conduct autonomous rendezvous and docking operations successfully, decades after the docking of the Soviet
Kosmos 186 and Kosmos 188 spacecraft in 1967.
Although it was originally intended to be used for 1.5 years, the satellite was functional for a period of almost five years.
ETS-VII eventually decayed from orbit on 13 November 2015.
Features
The ETS-VII consists of two main parts; the chaser satellite and the target satellite.
The chaser satellite is the main satellite body, and was named ''
Hikoboshi''. A 2 m long robotic arm was attached to this part. The smaller target satellite was named ''
Orihime''. The box shaped, complete satellite system weighed 2,860 kg.
The ETS-VII was equipped with three
solar panels
A solar panel is a device that converts sunlight into electricity by using photovoltaic (PV) cells. PV cells are made of materials that produce excited electrons when exposed to light. These electrons flow through a circuit and produce direct ...
, with two on the chaser satellite and one on the target satellite. The satellite was assisted by relative
global positioning system
The Global Positioning System (GPS) is a satellite-based hyperbolic navigation system owned by the United States Space Force and operated by Mission Delta 31. It is one of the global navigation satellite systems (GNSS) that provide ge ...
(RGPS) navigation.
Functioning
The satellite was launched using an
H-II rocket on 28 November 1997.
The launching took place at the
Tanegashima Space Center in Japan. The orbit of the ETS-VII was at an altitude of 550 km, with an inclination of 35 degrees.
The ETS-VII was built with an intended mission life of 1.5 years, with the mission to be ended in May 1999. However, in March 1999, it was decided to carry out operations for an additional six months because the satellite was in good condition. The last experiment carried out with the ETS-VII was ended on 16 December 1999. All the planned experiments had been carried out by this time, but the satellite was monitored to evaluate its durability. On 30 October 2002, the operating of the ETS-VII was terminated.
NASDA had invited research institutes in Japan and other countries to conduct joint experiments with the ETS-VII. As a result, joint experiments were conducted with organizations such as the
European Space Agency
The European Space Agency (ESA) is a 23-member International organization, international organization devoted to space exploration. With its headquarters in Paris and a staff of around 2,547 people globally as of 2023, ESA was founded in 1975 ...
(ESA).
Experiments
Three
rendezvous docking operations were carried out with the ETS-VII, which involved placing the target satellite 200 mm away from the chaser and using the robot arm to retrieve and hold it in place. Several other experiments were also carried out with the satellite's robotic components.
Most of the robot experiments were successfully completed by March 1999, and target satellite handling experiments were carried out in May 1999.
An error occurred during the second rendezvous docking operation which was carried out in August 1998. The
troubleshooting to identify this error was done in early March 1999. All previously planned robot experiments were completed by the end of March. Additional experiments were planned and carried out later.
The final rendezvous docking operation was successfully completed on 27 October 1999. The satellite's final robot experiment was carried out on 29 November. Satellite checkout was conducted as the last experimental operation on 15 and 16 December, concluding all operations carried out by the ETS-VII project team.
See also
*
Kosmos 186 and Kosmos 188
*
Orbital Express
Orbital Express: ASTRO and NEXTSat
Orbital Express was a space mission managed by the United States Defense Advanced Research Projects Agency (DARPA) and a team led by engineers at NASA's Marshall Space Flight Center (MSFC). The Orbital Express p ...
*
SPADEX (Space Docking Experiment)
*
Robotic Refueling Mission
References
External links
GIF animation of the docking
{{DEFAULTSORT:Ets-Vii
Satellites of Japan
Spacecraft launched in 1997
Spacecraft launched by H-II rockets
Spacecraft which reentered in 2015
Robotic satellite repair vehicles