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LUR 1 [AVS]
LUR 1 , designed by the Spanish company AVS, is a complete IOD (in orbit demonstration) space mission, to design, assembly, test, launch, and operate a satellite mission, including the Space Segment (SSEG), Ground Segment (GSEG) and User Segment (USEG).
The LUR-1 mission includes a satellite of 57 kg, built on AVS's LUR microsatellite platfor, with an Earth Observation payload. LUR-1 will also integrate the following IOD experiments and payloads:
- 1 unit of MICE (Mechanical Interface for Capture at EOL)
- 9 Proximity Operations Fiducial Markers
- 1 Retroreflector
- 1 SADA and complete deployable Solar Array including an SMA (Shape Memory Alloy) HDRM actuator developed by AVS
- 1 unit of QKD technology demonstrator including one single photon detector developed by AVS
- Communications: X-Band TX, S-Band TX/RX, and UHF TX/RX
- 1 Main Optical Payload for Earth imaging with a GSD of 1.5m
| Nation: | Spain |
|---|---|
| Type / Application: | Technology |
| Operator: | AVS |
| Contractors: | AVS |
| Equipment: | |
| Configuration: | LUR-bus |
| Propulsion: | |
| Power: | Solar cells, batteries |
| Lifetime: | |
| Mass: | 57 kg |
| Orbit: |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| LUR 1 | 2024-149AQ | 16.08.2024 | Va SLC-4E | Falcon-9 v1.2 (Block 5) | with Capella 15, Tyche, AWS, QPS-SAR 8, Van Zyl 1, Tanager 1, EagleEye, Umbra-SAR 09, 10, ICEYE X33, X39, X40, X43, ŅuSat 48, ..., 50, GNOMES 5, Hawk 10A, 10B, 10C, LUR 1, ION-SCV 012, Sedna 1, Lemur-2 193, ..., 196, Hubble 3, ERNST, CAKRA 1, BRO 14, 15, Connecta-IoT 1, ..., 4, CUAVA 2, Hyperfield 1A, HYPSO 2, Iperdrone.0, Kanyini, Lemu Nge, Φ-sat 2, PTD 4, PTD R, Sateliot 1, 2, 3, 4, Tomorrow S1, 2, TROOP F2, Waratah Seed 1, WREN 1, Flock-4be 1, ..., 36, GNA-3, Lemur-2 191, 192, Nightjar, QUBE, SATORO T2, TORO, UM5-EOSat, UM5-Ribat, Deimos, Lopen, Rock, OreSat 0.5, GaindéSat 1A, Pico 1B-1, ..., 9 |
Launch Sites:
- Va = Vandenberg Space Force Base, California, USA
