CubeSat
BACKGROUND:
The CubeSat team at UCI is a student-led effort to launch a 2U nanosatellite into orbit to test two UCI research payloads. The satellite operates with five subsystems (Power/Payload, Communications, Avionics, Structures/Thermal, and Systems Engineering), in addition to housing two payloads. The first payload is a variable emissivity device (VED) that will be tested as a thermal regulator, and our job is to test its performance in various degrees of solar exposure and at varying adjustable emissivity values. Similar materials to the sample are hoped to be used as a cheap method of thermal management on future spacecraft. The second payload is in collaboration with the ASPIN lab at UCI. The satellite will carry a transceiver meant to function as a transmitter of a “signal of opportunity”, helpful in researching novel navigation methods in the absence of or in place of a traditional GPS signal.
OBJECTIVES:
- Ensure that payload requirements ...






















