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AeroCube 10B

NSSDCA/COSPAR ID: 2019-022C

Description

Aerocube 10 (AC10) are a pair of 1.5U Cubesats developed by the Aerospace Corporation of El Segundo to demonstrate several technologies.

The purpose of the mission is to demonstrate precision satellite-to-satellite pointing; deployment of atmospheric probes for in-situ measurement of air density; small-spacecraft proximity operations using propulsion from a steam thruster (no docking is planned); and solar cell performance degradation experiment that will correlate data from radiation sensors tuned to the energy levels suspected of causing damage to a drop in solar cell power output.

The AeroCube-10B spacecraft replaces the payload volume area used for the dispenser on the 10A satellite with three different payloads. One is a steam propulsion unit identical to the one in AeroCubes-7b and 7c. It will dispense water vapor to create a 4 mN thrust to change the range between the two satellites. It holds up to 30 grams of water and can affect, best case a 10 meter per second delta velocity. Water is non-toxic and the pressure inside the steam propulsion unit is at atmospheric pressure, so it is not a pressure vessel. The other is an electron and proton spectrometer called the micro-Charged Particle Telescope (µCPT). It will measure radiation flux impinging on the satellite, in specific energy levels that are suspected to cause solar cell degradation. The third payload is a sensor that will confirm when the optical beacon is impinging on the satellite. It is a light sensor, tuned to the optical beacon and amplified because the intensity is predicted to be faint.

Alternate Names

    Facts in Brief

    Launch Date: 2019-04-17
    Launch Vehicle: Antares
    Launch Site: Wallops Island, United States

    Funding Agency

    • Unknown (United States)

    Discipline

    • Technology Applications

    Additional Information

    Questions and comments about this spacecraft can be directed to: Coordinated Request and User Support Office

     
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