Hamilton 1 is a 1U CubeSat space test flight of Kubos's flight control open-source flight control and mission management software.
The satellite contains a UHF/VFH radio transceiver, microcontroller-based flight computer, fixed body-mounted solar panels, electrical power system with 18650 LiPo batteries, and a magnetorquer-based attitude determination and control system. The satellite has a mass of 1.5 kg, and stowed dimensions of approximately 10 × 10 × 11 cm. Its expected orbital lifetime is approximately 18 years, with an active mission duration of 2 years. Post-mission disposal will be accomplished by uncontrolled atmospheric re-entry.
In space, Hamilton-1 will utilize, a full-duplex TRXVU commercial CubeSat radio, manufactured by Integrated Solutions In Space. The space radio will transmit on 449 MHz, via an isotropic dipole antenna with a peak gain of approximately 2 dBiC. The peak Equivalent Isotropic Radiated Power is 2 Watts (i.e, 33 dBm). The transmitted signal is GFSK-modulated, with a data rate of 9600 bps.
|Type / Application:||Technology|
|Power:||Solar cells, batteries|
|Hamilton 1||-||2018||Va SLC-4E||Falcon-9 v1.2||with SkySat 14, 15, Eu:CROPIS, STPSat 5, FalconSat 6, NEXTSat 1, KazSTSAT, eXCITe, SeeMe, ICEYE X2, BlackSky Global 2, ESEO, Hawk 1, 2, 3, Capella 1, AISTECHSAT 2, CSIM-FD, Hiber 2, ITASAT 1, Landmapper-BC 4, ROSE 1, ORS 7A, 7B, Al-Farabi 2, Astrocast 0.1, Audacy 0, BRIO, Centauri 2, Eaglet 1, Flock-3s 1, 2, 3, ICE-Cap, K2SAT, KazSciSat 1, MinXSS 2, Orbital Reflector, RAAF M1, SeaHawk 1, SNUSAT 2, THEA, VESTA, ZACUBE 2, PW-Sat 2, SNUGLITE, VisionCube, RANGE A, B, Elysium-Star 2, ExseedSat 1, Fox 1C, Irvine 02, JY1-Sat, KNACKSAT, MOVE 2, SpaceBEE 9, 10, 11, Suomi-100, WeissSat 1, BeeSat 5, 6, 7, 8, BlackHawk, ENOCH, SIRION Pathfinder 2, (US Gov), (US Gov), (US Gov), (US Gov), (US Gov)|