Prometheus-2 (original) (raw)

Prometheus Block 2 [LANL]

Prometheus is series of 1.5U CubeSats for technology development and demonstration. It was developed by the Los Alamos National Laboratory (LANL) with the dual objective of evaluating new low-cost development and operations methodologies while also assessing the operational utility that can be provided with CubeSat technology. It was DoD funded.

The Prometheus system consists of CubeSats along with supporting ground and field segment equipment, all designed as an integrated system. LANL is serving as the primary builder and system integrator and will perform on-orbit system checkout, test, and evaluation. The satellites were based on the earlier Prometheus and Perseus satellites. The Prometheus satellites cost less than $100,000 each, are expected to have a service life of three to five years and are demonstrating the capability to transfer audio, video, and data files from man-portable, low-profile, remotely located field units to deployable ground stations terminals using over-the-horizon satellite communications. Each satellite features four deployable solar arrays and a deployable helix antenna. The second generation Block 2 satellites feature several improvements. The solar arrays have been enlarged and the attitude control system has been improved. An star field sensor and a GPS receiver were added. Also they provide the opportunity for hosted payloads, as a 1.5U payload module can be added to each satellite.

Nation: USA
Type / Application: Technology
Operator: Los Alamos National Laboratory (LANL)
Contractors: Los Alamos National Laboratory (LANL)
Equipment:
Configuration: CubeSat (1.5U)
Propulsion: None
Power: 4 deployable fixed solar arrays, batteries
Lifetime: 3-5 years
Mass: 1.35 kg
Orbit: 572 km � 582 km, 97.97� (#2.1); 388 km � 602 km, 24.52� (#2.2); 572 km � 583 km, 97.98� (#2.3); 384 km � 603 km, 24.53� (#2.4); 300 km � 847 km, 28.53� (#2.6); 437 km � 460 km, 45.01� (#2.7); 489 km � 512 km, 60.69� (#2.8); 437 km � 460 km, 45.01� (#2.9); 519 km � 536 km, 97.51� (#2.10); 493 km � 514 km, 60.68� (#2.11)
Satellite COSPAR Date LS Launch Vehicle Remarks
Prometheus 2.1 2016-067G 11.11.2016 Va SLC-3E Atlas-5(401) with WorldView 4, RAVAN, OptiCube 4, AeroCube 8C, AeroCube 8D, Prometheus 2.3, CELTEE 1
Prometheus 2.2 ? 2017-050B ? 26.08.2017 CC SLC-46 Minotaur-4 Orion-38 with ORS 5, DHFR, Prometheus 2.4 ?
Prometheus 2.3 2016-067H 11.11.2016 Va SLC-3E Atlas-5(401) with WorldView 4, RAVAN, OptiCube 4, AeroCube 8C, AeroCube 8D, Prometheus 2.1, CELTEE 1
Prometheus 2.4 ? 2017-050C ? 26.08.2017 CC SLC-46 Minotaur-4 Orion-38 with ORS 5, DHFR, Prometheus 2.2 ?
Prometheus 2.5 - 202x with ?
Prometheus 2.6 2019-036AB 25.06.2019 CCK LC-39A Falcon-Heavy (Block 5) with DSX , FORMOSAT 7A, 7B, 7C, 7D, 7E, 7F, GPIM, OTB 1, NPSat 1, Oculus-ASR, Prox 1, LightSail 2, ARMADILLO, FalconSat 7, E-TBEx A, E-TBEx B, PSat 2, BRICSat 2, Prometheus Mass Model, TEPCE 1, 2, CP 9 (LEO), StangSat
Prometheus 2.7 2019-037K 29.06.2019 OnS LC-1A Electron KS with BlackSky Global 3, Painani 1, Prometheus 2.9, ACRUX 1, SpaceBEE 8, 9
Prometheus 2.8 2021-002N 17.01.2021 Mo RW12/30 LauncherOne with CACTUS 1, ExoCube 2, MiTEE 1, PolarCube, Q-PACE, TechEdSat 7, RadFxSat 2, CAPE 3, PICS 1, PICS 2, Prometheus 2.11
Prometheus 2.9 2019-037B 29.06.2019 OnS LC-1A Electron KS with BlackSky Global 3, Painani 1, Prometheus 2.7, ACRUX 1, SpaceBEE 8, 9
Prometheus 2.10 2021-006EH 24.01.2021 CC SLC-40 Falcon-9 v1.2 (Block 5) with Starlink v1.0 R1-1, ..., R1-10, QPS-SAR 2, Capella 3, 4, ICEYE X8, X9, XR 1, GHGSat C2, Hawk 2A, 2B, 2C, Sherpa-FX 1, ION-SCV 002, AII-Charlie, Hiber 4, ASELSAT, PIXL 1, SOMP 2b, IDEASSat, YUSAT 1, UVSQ-SAT, V-R3x 1, 2, 3, Flock-4s 1, ..., 48, Kepler 8, ..., 15, Astrocast 0101, ..., 0105, SpaceBEE 40, ..., 75, Lemur-2 130, ..., 137, PTD 1, ARCE 1A, 1B, 1C
Prometheus 2.11 2021-002E 17.01.2021 Mo RW12/30 LauncherOne with CACTUS 1, ExoCube 2, MiTEE 1, PolarCube, Q-PACE, TechEdSat 7, RadFxSat 2, CAPE 3, PICS 1, PICS 2, Prometheus 2.8

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