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Solar Cell Array 30% Triple Junction GaAs
| Category | Parameter | Mission Requirement | Expected Unit / Format |
| Volume | Number of units | 2–5 cells (research evaluation) | |
| Electrical (AM0) | BOL Efficiency | Manufacturer recommendation / datasheet value requested | % |
| EOL Efficiency | Not applicable (terrestrial research use) | % | |
| Max Power Voltage (Vmp) | Manufacturer datasheet requested | V | |
| Max Power Current (Imp) | Manufacturer datasheet requested | mA/cm² or A | |
| Open-Circuit Voltage (Voc) | Manufacturer datasheet requested | V | |
| Short-Circuit Current (Isc) | Manufacturer datasheet requested | mA/cm² or A | |
| Mechanical | Cell Architecture | Triple-junction (InGaP/GaAs/Ge) preferred | Text |
| Cell Dimensions | 40mm × 80 mm preferred ( or available options) | mm x mm | |
| CIC Assembly | Coverglass Thickness | Manufacturer recommendation | µm or mils |
| Coverglass Coatings | AR coating preferred | Text | |
| Interconnect Design | Manufacturer recommendation | Text | |
| Bypass Diode Type | Manufacturer recommendation | Text | |
| Contact Layout | Manufacturer recommendation | Text | |
| Heritage & QA | Flight Heritage | Not required for terrestrial research | Orbit / Mission List |
| Space Standard Auth. | Not required | Text | |
| LAT Documentation | Preferred if available | Yes/No |
Status:
Open
12U structure
RFI for a 12U structure
Status:
Open
AIS Payload
We are looking for a AIS Payload, preferably VDES 2.0.
Min TRL 8.
Status:
Open
Solar Array Drive Assembly
| SOLAR ARRAY DRIVE ASSEMBLY (SADA) - PROCUREMENT SPECIFICATION | |||
| Category | Parameter | Input Value / Target | Unit / Notes |
| PROJECT INFORMATION | |||
| Project / Mission Name | GEO | E.g., Earth Obs Constellation, GEO Commsat | |
| Target Orbit | GEO | LEO, MEO, GEO, Deep Space | |
| SUPPLY CHAIN & LOGISTICS | |||
| Quantity Required (Flight) | 2 | Number of flight units (per spacecraft) | |
| Quantity Required (Eng/Qual) | 1 | Number of EM/QM/STM units | |
| Target Lead Time (ARO) | 12 | [Months] Time from Order to Delivery | |
| Export Control Classification | None | ITAR, EAR, or ECCN code | |
| Technology Readiness Level (TRL) | TRL 9 (Flight Proven) | TRL 1-9 (Prefer TRL 8+ for mechanisms) | |
| SLIP RING & POWER TRANSFER | |||
| Power Transfer Architecture | Slip Ring (Continuous 360) | Continuous Slip Ring vs. Cable Wrap/Twist Capsule | |
| Maximum Bus Voltage | 42 | [Vdc] E.g., 28V, 50V, 100V | |
| Total Power Transfer Required | 400 | [W or kW] Total solar array power passing through SADA | |
| KINEMATICS & MOTOR CONTROL | |||
| Drive Motor Type | Stepper Motor | Stepper Motor, Brushless DC (BLDC) | |
| Rotation Range | Continuous 360 Degrees | Continuous 360°, Limited Angle (e.g., ±180°) | |
| MECHANICAL & LOAD CAPACITIES | |||
| Maximum Mass | 7 | [kg] Mass of SADA (Motor + Slip Ring + Housing) | |
| ENVIRONMENTAL & SURVIVABILITY | |||
| Required Operational Life | 5 | [Years] Mission duration | |
Status:
Open
2U CubeSat Structure
RFQ for 2U CubeSat Structure
Status:
Open
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