|Mission type||Earth imaging|
|Mission duration||60 - 90 days (planned)|
|Spacecraft type||1U CubeSat|
|Launch mass||1.3 kg (2.9 lb)|
|Start of mission|
|Launch date||9 January 2014, 18:07:05 UTC|
|Launch site||MARS, LP-0A|
|Deployed from||International Space Station|
|Deployment date||28 February 2014|
|End of mission|
|Last contact||27 March 2014|
|Decay date||9 November 2014|
|Reference system||Geocentric orbit |
|Regime||Low Earth orbit|
|Perigee altitude||408 km (254 mi)|
|Apogee altitude||414 km (257 mi)|
SkyCube was an American crowdsourced CubeSat. It was first announced on Kickstarter on 14 July 2012 and successfully funded on 12 September 2012, meeting its US$82,500 goal with a total of US$116,890. It was developed and built in 2012–2013, completed flight integration at Nanoracks in late 2013, and finally launched aboard the Cygnus CRS Orb-1 flight at the Mid-Atlantic Regional Spaceport on Wallops Island, Virginia on 9 January 2014. SkyCube was deployed from the International Space Station on 28 February 2014. Contact with the satellite was last made on 27 March 2014. SkyCube re-entered the Earth's atmosphere on 9 November 2014. It is one of several crowdfunded satellites launched during the 2010s.
SkyCube had three major mission components: the broadcast of messages from its radio, the capture of pictures from space via its three cameras, and the deployment of a large balloon.
The SkyCube radio emitted periodic beaconing pings which contained 120-byte messages from the Kickstarter backers. These pings were transmitted at 915 MHz, using the AX.25 protocol at 9600 baud with BPSK modulation, with a callsign of WG9XMF.
Using its three cameras, SkyCube took pictures of the Earth from orbit. The cameras were VGA resolution and had lenses with three different fields of view (120°, 35°, and 6°), giving a variety of imaging possibilities. The images were transmitted back to Earth at 57.6 kbit/s. Kickstarter backers chose when the pictures were taken. National Oceanic and Atmospheric Administration (NOAA) granted a 90-day imaging license to SkyCube on 1 February 2013.
SkyCube deployed a large (2 m (6 ft 7 in)) balloon at the end of its mission. The balloon was coated with reflective titanium dioxide and made it visible from the ground. The balloon increased the atmospheric drag on SkyCube, and within two weeks the orbit decayed enough for SkyCube to enter Earth's atmosphere and burn up safely. The inflation was triggered via 4-gram CO2 canister.
|Dimensions||10 × 10 × 11.3 cm CubeSat standard|
|Interface specification||ISIPOD 1.4I|
|Mass||1.3 kg (2.9 lb)|
|Expected lifetime||60 – 90 days|
|Attitude control system||Passive magnotorquers|
|Power||9 total panels: one roof panel and 8 deployable panels. Each panel consists of 24 Spectrolab triangular cells wired in series-parallel for a nominal 12 V.|
|Batteries||2 x Li-ion 18650 cells, 8.4 V 2300 mAh, Molicell ICR18650J.|
|Power bus||3.3 V, 5 V regulated. Constant-current driver for solar panel deployment (Nichrome burn wires).|
|Primary downlink||915 MHz, AX.25 protocol, BPSK modulation, 57.6 kbit/s|
|Telemetry/messaging downlink||915 MHz, AX.25 protocol, BPSK modulation, 9.6 kbit/s|
|Command uplink||450 MHz, AX.25 protocol, FSK modulation, 9.6 kbit/s|
SkyCube relied on several partners to provide necessary services:
|Naval Postgraduate School||Ground station services in North America and Hawaii |
|Saber Astronautics||Ground station and Mission Control services in Australia |
|Orbital Sciences||Launch provider|
|Astronautical Development, LLC||Radios and structural components|