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Cubesat optical communication terminal
A qualified satsearch buyer has submitted an RFQ for a CubeSat optical communication terminal - for the space to ground link.
If you are interested in this business opportunity please contact us today using the button below.
Status:
Open
Ka-band SSPA
5U SSPA with 34GHz-36GHz output power greater than 53dBm
Status:
Open
OCT
| Section | Parameter | Minimum Buyer Requirement / Value | Notes / Document Reference |
| Project / Mission Requirements | Required Delivery Date (Flight) | 2028 | e.g., Q3 2028 |
| Quantity Required | TBD | e.g., 2 Flight Units + 1 Engineering Model | |
| Target Cost Per Unit | - | e.g., $400,000 | |
| Mission Lifetime | 5 Years | e.g., 5 Years | |
| Target Orbit / Altitude | LEO / 600-800 km | e.g., LEO / 550 km Sun-Synch | |
| 2. Technical - Optical | Laser Wavelength | 1550 nm | e.g., 1550 nm (C-band) |
| Interoperability Standard | SDA Tranche 1 | e.g., SDA Tranche 1 / CCSDS | |
| 2. Technical - Performance | Data Rate (Tx / Rx) | 1- 10 Gbps | e.g., 2.5 Gbps / 2.5 Gbps |
| Link Distance (Range) | Up to 5,000 km | e.g., Up to 5,000 km | |
| 2. Technical - SWaP-C | Mass (Weight) | ≤ 10 kg | e.g., < 15 kg |
| Power Consumption (Peak) | < 75 W | e.g., < 80 W (Operational) | |
| Volume / Envelope Dimensions | < 250 x 250 x 250 mm | e.g., 300 x 250 x 200 mm | |
| 2. Technical - Interfaces | Data Interface | Ethernet | e.g., SpaceWire / OIF / Ethernet |
| Electrical / Power Input | 28 VDC regulated | e.g., 28V DC regulated | |
| Mechanical Mounting | TBD | e.g., 4x M5 bolts, nadir-facing | |
| 2. Technical - Pointing | Field of Regard (FoR) | TBD (Optics will be decided later) | e.g., Azimuth: ±90°, Elevation: ±45° |
| 3. Environmental | Technology Readiness Level (TRL) | at least TRL 6-7 | Minimum TRL 6 (Flight proven preferred) |
| Operational Temperature | LEO conditions | -20°C to +55°C | |
| Survival Temperature | -40°C to +75°C | ||
| Random Vibration (Launch) | TBD (Launch Vehicle specs) | e.g., 14.1 grms (or specific launch vehicle spec) | |
| Radiation Tolerance (TID) | TBD (Will be similar for LEO 600 - 800 km) | e.g., 30 krad (Si) absorbed dose | |
| Component Screening Level | TBD | e.g., NASA Level 2 / ECSS Class 2 | |
| 4. Deliverables | 3D CAD Model (STEP format) | Yes | Required at Preliminary Design Review (PDR) |
| Electrical Interface Control Document (ICD) | Yes | Required at Critical Design Review (CDR) | |
| Software/Firmware ICD | Yes | Required at Critical Design Review (CDR) | |
| Thermal / Structural FEA Models | Yes | Required at Critical Design Review (CDR) | |
| End-of-Line Test Reports | Yes | Required prior to shipment | |
| Certificate of Conformance (CoC) | Yes | Required at delivery |
Status:
Open
Payload hosting
| # | Parameter | Requirement | Response |
| 1 | Physical Properties | Payload Mass (kg) | 2.3 kg |
| 2 | Payload Volume (U or m3) | 1.5U | |
| 3 | General | Payload type e.g. RF, EO (RGB, HS, MS IR) | SSA |
| 4 | Desired orbits e.g. SSO, near-equatorial | Mid-Inclination (preferred), or SSO | |
| 5 | Desired altitudes e.g. 550 km | 500-550 km | |
| 6 | EPS | Payload continuous power (W) | 25W |
| 7 | Payload peak power (W) | 40W | |
| 8 | Payload duty cycle per orbit (%) | TBD with the provider | |
| 9 | Payload voltage supply e.g. 3V3, 5V, 12V | 12-36 V | |
| 10 | RF | High-speed downlink required e.g. > 5 Mbps? | X-Band (preferred), S-Band (minimum requirement) |
| 11 | Daily data budget (Mb or Gb) | TBD | |
| 12 | Encryption required on TTC or payload data e.g. AES-256? | ||
| 13 | Interfaces | Bus to payload interfaces required e.g. CAN, I2C, SPI, UART, RS422, RS485, PPS | CSP 1.6 over CAN & UART
|
| 14 | On-board data storage requirements? | No on-board data storage required | |
| 15 | ADCS | Payload Pointing Modes when active e.g. Nadir | Nadir Pointing, Satellite Tracking (optional) |
| 16 | Pointing Accuracy | Better than 1 deg/s | |
| 17 | Pointing Knowledge | Better than 0.5 deg/s | |
| 18 | Slew Rate (°/s) requirements? | ||
| 19 | GPS required for position, velocity knowledge? | GNSS log is required during operation |
Status:
Open
Pre-heating
Pre-heating solutions for thruster propellant
Status:
Open
S-band transceivers
Searching for a CCSDS-compatible S-band transceivers.
Uplink shall comply to CCSDS 231.0-B-4 & 232.0-B-4. For channel coding, only BCH coding is required. BCH may operate in checksum mode (ie: SECDED mode is not required). If part of the framing layer needs to be implemented on the customer side, that is acceptable, as long as the unit at minimum extracts transfer frames. Uplink data rate up to 100 kbps.
Downlink shall comply to CCSDS 131.0-B-6 & 132.0-B-3. For channel coding, 1/2 rate convolutional coding + RS(255,233) w/interleaving is required. If part of the framing layer needs to be implemented on the customer side, that is acceptable, as long as the unit can consume transfer frames. Downlink data rate up to 1 Mbps.
TID hardening is not required, but the system shall be resilient to SEEs (ie: SEU, SEL) up to 600 km.
Looking to procure 5 EMs & 5 FMs. If the unit operates satisfactorily, this may lead to a long-term engagement of 5-10 FMs/year starting in 2030.
Status:
Open
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