Dove 1, 2

The Dove-1 mission is a technology demonstration nanosatellite based on the triple CubeSat form factor:

The goal of the mission is:

  • build a low-cost imaging satellite with non-space, COTS components;
  • to show that a bus constrained to the 3U cubesat form factor can viably host a small camera payload; and
  • demonstrate the ability to design, produce and operate satellites on short schedules and low cost.

Dove-1 will do this by transmitting health and image data to the ground.

The satellite will be launchd as a secondary payload on the maiden flight of the Antares-110 launch vehicle in 2012.

The Dove 2 mission is also an internal company technology demonstration experiment to test the capabilities of a low-cost spacecraft constrained to the 3U cubesat form factor to host a small payload. It will be launched in 2012 as a piggyback payload on a Soyuz-2-1b launch.

Nation: USA
Type / Application: Technology
Operator: Cosmogia Inc.
Contractors:
Equipment:
Configuration: CubeSat (3U)
Propulsion: none
Power: Solar cells, batteries
Lifetime: ~14 days (#1); ~180 days (#2)
Mass: 5.5 kg
Orbit: 280 km × 270 km, 51.6°
Satellite Date LS Launch Vehicle Remarks
Dove 1 2012 WI LC-0A Antares-110 with Cygnus mass model, PhoneSat v1a, PhoneSat v1b, PhoneSat v1c
Dove 2 2012 TB LC-31/6 Soyuz-2-1b with Bion-M 1