Microgravity Experiment System using High altitude Balloon

*BOV :Balloon-based Operation Vehicle

Microgravity experiment system using high altitude balloon(BOV :Balloon-based Operation Vehicle)

 In order to fulfill the gap between short-term microgravity experiment system (parabolic flight and drop tower) and long-term one (the International Space Station) , a new system using a high altitude balloon (BOV :Balloon-based Operation Vehicle) has been developed.
A combustion experiment (Combustion of Japanese sparker in microgravity) was conducted in the second flight of BOV in May, 2007.


High altitude balloon

BOV#4 In order to get low gravity condition (10-4G) around 30 seconds, free fall from as high as 40Km above sea level was required. To reach such a high altitude, a high altitude balloon was utilized. Helium gas was filled in the balloon, and altitude of the balloon was controlled using gas exhaust mechanism and ballast release system.
The balloon flew east by eastbound wind while the balloon was in low altitude, and return west by westbound wind in high altitude. When the balloon reached the pre-determined position, a free fall capsule (BOV) was released from the balloon.

balloon launch →ballast→microgravity experiment→retrievel

Details of the microgravity experiment section in BOV

 In order to get better gravity level, the microgravity experiment section is levitating inside the BOV. Therefore, the experiment section has to contain its own power supply, control system, etc. Command and telemetry from/to ground should be transferred wirelessly, via BOV. Every component of the experiment system was packed in the sphere whose diameter was 28 cm.

  • Microgravity experiment section

    Microgravity experiment section
    Size of the experiment section is 28 cm in diameter, as big as a bowling ball. Both north and south hemisphere are covered with polycarbonate shell. South hemisphere is painted yellow for the sake of drag free control by BOV. ( p1 / 12 )

  • Combustion chambe

    Combustion chamber
    The combustion chamber was a cube made of stainless steel. It was filled with 4.5 atm air.( p2 / 12 )

  • A Japanese sparker (red) in the feed through

    A Japanese sparker (red) in the feed through
    A Japanese sparker was tied with Cr-Fe wire, thorough which ignition current was going. ( p3 / 12 )

  • Japanese sparker after the microgravity experiment

    Japanese sparker after the microgravity experiment( p4 / 12 )

  • Accelerometer

    Accelerometer (black cube)
    Structure of the experiment section was made of aluminum alloy. ( p5 / 12 )

  • Top of the north hemisphere

    Top of the north hemisphere
    Wireless RS-232C transmitter/receiver, IR receiver, wireless video transmitter are located.( p6 / 12 )

  • PIC for experiment control

    PIC for experiment control
    Experiment sequence was controlled by PIC controllers. Combustion video was recorded using a handy video recorder.( p7 / 12 )

  • Lucky charm

    A lucky charm was put in the experiment section.( p8 / 12 )

  • Microgravity experiment section

    Microgravity experiment section was placed inside the BOV. ( p9 / 12 )

  • Microgravity experiment section

    The microgravity experiment section will levitate in the BOV. A closure panel is about to be closed. ( p10 / 12 )

  • BOV

    BOV (the microgravity experiment section is located around the red line)( p11 / 12 )

  • BOV

    BOV is about to connected to the balloon( p12 / 12 )

BOV Menu

Takehiko Ishikawa
Department of Interdisciplinary Space Science / ISAS / JAXA
About ISAS > Academic Staff
» JAXA Repository

JAXA’s Tsukuba Space Center (TKSC)
2-1-1 Sengen, Tsukuba-shi, Ibaraki 305-8505
outbound link About TKSC
outbound link TKSC Access

Takehiko Ishikwa

outbound link(JAXA・ELF)