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Landmapper-Demo 6, 7

Landmapper-Demo 6 [Astrp Digital]

Astro Digital's Landmapper-Demo is a technology demonstration mission consisting of two separate, identical spacecraft: Landmapper-Demo 6 (Demo 6)and Landmapper-Demo 7 (Demo 7).

Each of the 870 kg spacecraft includes two payloads: an optical communication system and a high-performance payload data processor. The spacecraft bus is the Corvus-XL design. The common satellite bus uses reaction wheels, magnetic torque coils,star trackers, magnetometers, sun sensors, and gyroscopes to enable precision 3-axis pointing. The satellites have an electric propulsion system and a mono-propellant chemical thruster to provide functional redundancy at the mission level for orbital maneuvers.

Nation: USA
Type / Application: Technology
Operator: Astro Digital
Contractors: Astro Digital
Equipment: optical communication system, high-performance payload data processor
Configuration: Corvus-XL
Propulsion: None
Power: Solar cells, batteries
Lifetime:
Mass: 81 kg
Orbit:
Satellite COSPAR Date LS Launch Vehicle Remarks
Landmapper-Demo 6 - 2021 CC SLC-40 Falcon-9 v1.2 (Block 5) with Starlink v1.0 R1-1, ..., R1-10, QPS-SAR 2, Umbra-SAR 2001, Capella 3, 4, ICEYE X8, X9, X10, XR 1, Landmapper-Demo 7, GNOMES 2, GHGSat C2, Hawk 2A, 2B, 2C, SHERPA-FX 1, ION-SCV 2, SAMSON 1, 2, 3, Charlie, ASELSAT, PIXL 1, LINCS A, B, SOMP 2b, UVSQ-SAT, CPOD A, B, Astrocast 1.x1, ..., 1.x5, SpaceBEE x1, ..., x24, PTD 1, Lemur-2 130, ..., 137, Prometheus-2 10, ARCE 1A, 1B, 1C, (multiple satellites)
Landmapper-Demo 7 - 2021 CC SLC-40 Falcon-9 v1.2 (Block 5) with Starlink v1.0 R1-1, ..., R1-10, QPS-SAR 2, Umbra-SAR 2001, Capella 3, 4, ICEYE X8, X9, X10, XR 1, Landmapper-Demo 6, GNOMES 2, GHGSat C2, Hawk 2A, 2B, 2C, SHERPA-FX 1, ION-SCV 2, SAMSON 1, 2, 3, Charlie, ASELSAT, PIXL 1, LINCS A, B, SOMP 2b, UVSQ-SAT, CPOD A, B, Astrocast 1.x1, ..., 1.x5, SpaceBEE x1, ..., x24, PTD 1, Lemur-2 130, ..., 137, Prometheus-2 10, ARCE 1A, 1B, 1C, (multiple satellites)