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FUNcube

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FUNcube
NameFUNcube
Mission typeTechnology demonstration, Amateur radio, Education
OperatorAMSAT-UK, ESA Education Office
Mission durationPlanned: 1 year, Elapsed: 10+ years
Spacecraft busCubeSat (1U)
ManufacturerAMSAT-UK, University of Surrey
Launch mass1 kg
PowerSolar cells on body, Lithium-ion battery
Launch date21 November 2013, 07:10 UTC
Launch rocketDnepr
Launch siteDombarovsky (air base)
Entered serviceDecember 2013
Orbit referenceGeocentric orbit
Orbit regimeSun-synchronous orbit
Orbit periapsis588 km
Orbit apoapsis666 km
Orbit inclination97.8°
Orbit period97.4 minutes
Apsisgee

FUNcube is a pioneering CubeSat project designed primarily for educational outreach and amateur radio communication. Developed through a collaboration between AMSAT-UK and the University of Surrey, with support from the ESA Education Office, it was launched in 2013 as part of a broader Dnepr cluster mission. The satellite's core mission is to engage schools and radio enthusiasts worldwide by providing a simple, accessible platform for receiving telemetry and conducting basic space science experiments. Its longevity and reliability have made it a cornerstone in the global amateur satellite community.

Overview

The FUNcube project represents a significant initiative in the field of space education and citizen science. As a fully functional 1U CubeSat, it operates on amateur radio frequencies, allowing it to be received with relatively inexpensive ground station equipment. The project is managed by a dedicated team of volunteers from AMSAT-UK and leverages expertise from the Surrey Space Centre. Its design philosophy emphasizes simplicity and robustness, enabling it to serve as an educational tool for demonstrating orbital mechanics, radio wave propagation, and spacecraft telemetry principles to students.

Development and Launch

Development of the satellite began in the late 2000s, spearheaded by members of AMSAT-UK in partnership with the University of Surrey. Key technical contributions came from the Surrey Satellite Technology Ltd (SSTL) knowledge base. The spacecraft bus is a standard CubeSat structure, with critical subsystems including a UHF transmitter, a VHF receiver, and a suite of sensors. After successful integration and testing, it was launched on 21 November 2013 aboard a Kosmotras Dnepr rocket from Dombarovsky (air base) in Russia. The launch was part of the larger QB50 precursor mission, deploying multiple small satellites into a sun-synchronous orbit.

Mission and Educational Objectives

The primary mission is to stimulate interest in science, technology, engineering, and mathematics (STEM) subjects. It achieves this by transmitting continuous telemetry containing data on its internal temperature, solar panel output, and battery voltage, which can be decoded by students using a simple software-defined radio dongle. The project provides extensive online resources, lesson plans, and support through the AMSAT network. A key objective is to allow participants to collect real data from space, fostering practical understanding of subjects like physics and electronics, and linking to curriculum topics such as the Kennedy Space Center Visitor Complex's education programs.

Technical Specifications

The satellite conforms to the standard 1U CubeSat dimensions of 10x10x10 cm. Its communications payload includes a 435 MHz UHF downlink for telemetry and a 145 MHz VHF uplink for commanding. Power is generated by body-mounted triple-junction solar cells and stored in a lithium-ion battery pack. The onboard computer, based on a Texas Instruments MSP430 microcontroller, manages subsystems and the beacon transmitter. The payload also includes a MEMS thermometer and photodiodes to measure light levels, with data formatted in the standardized AX.25 packet radio protocol for amateur radio.

Operational History

Following its successful deployment, the satellite was activated and began transmitting its beacon signal, which was quickly acquired by the global network of amateur radio operators. Despite an initial issue with its VHF receiver, which limited commanding capabilities, the robust UHF downlink has remained operational for over a decade, far exceeding its planned one-year mission. It has been used in countless school projects, featured at events like the Dayton Hamvention, and supported initiatives by the Radio Society of Great Britain. Its enduring operation has provided invaluable long-term data on CubeSat longevity and has cemented its status as a vital educational asset within the International Space Station (ISS) ham radio community.

Category:CubeSats Category:Amateur radio satellites Category:Spacecraft launched in 2013 Category:AMSAT