Leads
Bid on open business opportunities for space products or services
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Hinge for Small Satellites
RFQ for hinges that can support a 1.5 m^2 solar panel (using 2 hinges per panel).
The hinges would attach to a rigid plate on the spacecraft, stowed at 90 degrees, deployed at 180 degrees.
Would need engineering units by May 2024 and flight units by June 2024.
Status:
Open
RFP for TNC Connectors
A well qualified buyer from Spain is looking for 4 flight TNC connectors to handle 20W of RMS and 70W peak power at 115 MHz.
The buyer is working on a short operating timeline of less than 4 months would like a quotation for 4 FMs and 8 EMs.
Do you have a TNC connector that can satisfy these mission requirements?
If so, please click the button below to find out how to access this opportunity.
Status:
Open
RFQ for X-Band Transmitter
A well qualified buyer is looking for a quotation for an X-band transmitter with the following specifications:
- Flight model
- Carrier frequency: from 8025 MHz to 8400 MHz
- Data rate: not less than 50 Mbps
- Modulation: OQPSK
- Coding: Convolutional Coding (2/1, 7)
- Output power: Not less than 33 dBm
- Maximum power consumption: Not more than 11W
- Transmitted data: Compatible with CCSDS AOS Standard
- Control interface: RS422 (Preferred)
- Data interface: LVDS
- Antenna interface: 50 Ohm SMP male connector
- DSN filter: 40 dB attenuation at 8400 MHz
Do you have an X-band transmitter that can satisfy these requirements?
If so, please click the button below to find out how to access this opportunity.
Status:
Open
RFP for Power Control and Distribution Unit (PCDU) for a microsat constellation
A qualified and well-funded organization is looking to build a 3 satellite constellation for a LEO mission. The organization is institutional, working closely with a prominent private party in industry.
The organization intends to finalise the Preliminary Design Review (PDR) by the end of Q1 2024 and launch in Q3 2026.
This prospective buyer is currently actively looking for a PCDU for a microsatellite platform (180 kgs), with peak power generation of at least 200 W.
The minimum lifetime of the mission is 5.5 years.
Do you have a PCDU that can satisfy these mission requirements?
If so, please click the button below to find out how to access this opportunity.
Status:
Open
RFP for a sun sensor simulator
A scale-up based in India is looking for a sun sensor simulator for immediate procurement.
The simulator is to provide stimuli on a coarse sun sensor, to test it's functionality and expected performance in upcoming satellite missions.
The buyer is operating on a short timeline and is requesting delivery in Q1 2024.
Do you have a sun sensor simulator that can satisfy these mission requirements?
If so, please click the button below to find out how to access this opportunity.
Status:
Open
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