The information compiled and edited in this article was provided by Herbert J. Kramer from his documentation of: ”Observation of the Earth and Its Environment: Survey of Missions and Sensors” (Springer Verlag) as well as many other sources after the publication of the 4th edition in 2002.

When a GRB is detected, the onboard CPU calculates the coordinate and then the satellite slews rapidly using the CMG (Control Moment Gyro). In order to determine the position of the transient object, the detectors are pointed into five different directions. 11): 1) Detumbling mode (occurs after spacecraft deployment).

The CGM development is discussed separately (see Experiment/sensor complement). This caused a loss of contact with the ground station. $(function(){ In fact, the depth of discharge was no more than 50% in the flight operation. The geometrical structure of the HXCP was designed based on Monte-Carlo simulations to achieve high sensitivity in spite of its small effective area. Failure analyses and design improvements are in progress. Tsubame (Demonstration Microsatellite of TITech, Tokyo), Overview    Spacecraft    Launch    Mission Status    Sensor Complement   References, Tsubame is a science and technology demonstration mission developed by a student-lead system design of the Matunaga LSS (Laboratory for Space System) at the Tokyo Institute of Technology (referred to as TITech or simply Tokyo Tech).

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The information compiled and edited in this article was provided by Herbert J. Kramer from his documentation of: ”Observation of the Earth and Its Environment: Survey of Missions and Sensors” (Springer Verlag) as well as many other sources after the publication of the 4th edition in 2002.

When a GRB is detected, the onboard CPU calculates the coordinate and then the satellite slews rapidly using the CMG (Control Moment Gyro). In order to determine the position of the transient object, the detectors are pointed into five different directions. 11): 1) Detumbling mode (occurs after spacecraft deployment).

The CGM development is discussed separately (see Experiment/sensor complement). This caused a loss of contact with the ground station. $(function(){ In fact, the depth of discharge was no more than 50% in the flight operation. The geometrical structure of the HXCP was designed based on Monte-Carlo simulations to achieve high sensitivity in spite of its small effective area. Failure analyses and design improvements are in progress. Tsubame (Demonstration Microsatellite of TITech, Tokyo), Overview    Spacecraft    Launch    Mission Status    Sensor Complement   References, Tsubame is a science and technology demonstration mission developed by a student-lead system design of the Matunaga LSS (Laboratory for Space System) at the Tokyo Institute of Technology (referred to as TITech or simply Tokyo Tech).

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Furthermore, we are developing a compact satellite to minimize air resistance, and will verify that our technology can support orbiting at super low altitudes over an extended period of time. Table 3: Specification of the optical camera, The objective is to provide GRB (Gamma-Ray Burst) observations with the agile Tsubame spacecraft.

Legend to Figure 20: The scintillators and detectors are accommodated in an upward direction, the passive shields surround them.

The Laboratory for Space Systems is responsible for the overall running of the project, development, test, launch and operation as well as for the specific development of the satellite bus system. The nature of GRBs (Gamma Ray Bursts) is generally of short duration (events on the order of 1 minute); in addition, GRBs happen to be unpredictable events to occur anywhere within the celestial sky. A CMG can produce larger torque than conventional actuators such as reaction wheels. A "super low orbit" refers to an orbit with an altitude lower than 300 km. data rate of 100 kbit/s (BPSK modulation). Following the launch of the LSS’s third satellite, Cute-1.7 + APD II, the TSUBAME project was initialised and is currently in the BBM (Bread Board Model) development phase.

The information compiled and edited in this article was provided by Herbert J. Kramer from his documentation of: ”Observation of the Earth and Its Environment: Survey of Missions and Sensors” (Springer Verlag) as well as many other sources after the publication of the 4th edition in 2002.

When a GRB is detected, the onboard CPU calculates the coordinate and then the satellite slews rapidly using the CMG (Control Moment Gyro). In order to determine the position of the transient object, the detectors are pointed into five different directions. 11): 1) Detumbling mode (occurs after spacecraft deployment).

The CGM development is discussed separately (see Experiment/sensor complement). This caused a loss of contact with the ground station. $(function(){ In fact, the depth of discharge was no more than 50% in the flight operation. The geometrical structure of the HXCP was designed based on Monte-Carlo simulations to achieve high sensitivity in spite of its small effective area. Failure analyses and design improvements are in progress. Tsubame (Demonstration Microsatellite of TITech, Tokyo), Overview    Spacecraft    Launch    Mission Status    Sensor Complement   References, Tsubame is a science and technology demonstration mission developed by a student-lead system design of the Matunaga LSS (Laboratory for Space System) at the Tokyo Institute of Technology (referred to as TITech or simply Tokyo Tech).

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