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Real-Time Buyer Demand
See the latest inquiries from engineers and organizations actively seeking spacecraft components
S-band transceiver
CommunicationsLooking for S-band transceiver capable of 10 Mbps data rate for LEO satellite constellation.
Solar panel arrays
Power SystemsHigh-efficiency solar panels for small satellite missions, minimum 200W output.
Attitude control thrusters
PropulsionCold gas thrusters for 3U CubeSat attitude control, 1N thrust capability.
Star tracker sensors
NavigationHigh-precision star tracker for deep space navigation, 0.1 arcsecond accuracy.
Thermal control systems
Thermal ManagementPassive thermal control coatings for Mars orbiter mission.
Data storage units
Data SystemsRadiation-hardened solid state drives, minimum 1TB capacity.
Antenna deployment mechanisms
Mechanical SystemsReliable deployment system for deployable mesh antennas.
Battery management systems
Power SystemsLithium-ion battery management for long-duration missions.
X-band payload antenna
CommunicationsLooking for X-band high-gain antenna for 1 Gbps downlink from GEO.
Radiation shielding materials
MaterialsLightweight composite shielding for CubeSats operating in MEO.
Onboard computer (OBC)
Data SystemsFault-tolerant OBC with ARM processor and at least 2GB RAM.
Deployable solar wings
Power SystemsCompact solar wing array with >30% efficiency for microsatellite bus.
Reaction wheels
Attitude ControlSmall reaction wheel assembly for CubeSats, torque up to 0.005 Nm.
Chemical propulsion system
PropulsionMiniature monopropellant system providing 5N thrust for orbital maneuvers.
Deployable drag sails
Deorbit SystemsEnd-of-life deorbit drag sail for 6U CubeSat compliance.
High-speed SDR
CommunicationsSoftware-defined radio capable of Ka-band uplink and downlink.
Sun sensors
NavigationCoarse sun sensors for CubeSat ACS with <5° accuracy.
Li-ion batteries
Power SystemsSpace-qualified 20Ah lithium-ion battery pack for LEO missions.
Deployable booms
StructuresLightweight composite booms for magnetometer deployment.
Cryocoolers
Thermal ManagementMiniature cryocooler for IR detector cooling to 80K.
GNSS receivers
NavigationMulti-constellation GNSS receiver for LEO, timing accuracy <20ns.
Plasma thrusters
PropulsionHall-effect thruster suitable for 200kg spacecraft, Isp > 1500s.
Magnetorquers
Attitude ControlThree-axis magnetorquer rods for CubeSat detumbling.
High-gain parabolic antennas
CommunicationsDeployable reflector antenna for Ka-band comms.
Power distribution unit
Power SystemsRadiation-tolerant PDU for small satellite buses.
Optical communications terminals
CommunicationsLasercom terminal for LEO-to-ground 1 Gbps data rate.
Thermal straps
Thermal ManagementFlexible graphite thermal straps for heat transfer from payload to radiator.
CubeSat structures
StructuresStandardized 12U structure compatible with CubeSat deployers.
Earth observation cameras
PayloadsHigh-resolution imager with 1m GSD for EO missions.
Deployable landing legs
Mechanical SystemsCompact shock-absorbing legs for lunar micro-lander.
Onboard AI processors
Data SystemsRadiation-tolerant AI/ML edge computing module for EO image processing.
ISL terminals
CommunicationsInter-satellite link laser terminal with >1000 km range.
Propellant tanks
PropulsionLightweight composite propellant tanks for 10 bar pressure rating.
Ground station antennas
Ground SystemsPortable S/X-band ground station dish for field deployments.
Deployable reflectors
PayloadsLarge deployable reflector for synthetic aperture radar (SAR).
Flight software
SoftwareAutonomous flight software for CubeSat bus, modular architecture.
Radiators
Thermal ManagementLightweight deployable radiators for LEO spacecraft thermal control.
Space-rated connectors
ComponentsMicro-D connectors rated for vacuum and radiation.
Docking mechanisms
Mechanical SystemsSmall sat docking adapter for on-orbit servicing.
Launch adapters
StructuresMulti-satellite launch adapter for rideshare missions.
Space tethers
Deorbit SystemsElectrodynamic tether for deorbit applications.
Radiation-hardened processors
Data SystemsQuad-core processor hardened for GEO mission lifetimes.
Optical sensors
PayloadsWide-angle optical payload for SSA applications.
RF switches
CommunicationsHigh-power RF switches for satellite communication payloads.
Vibration isolation systems
Mechanical SystemsPassive isolation mounts for optical payload stability.
Deployable antennas
CommunicationsTape-spring antenna for UHF CubeSat communications.
Thermal vacuum chambers
Test EquipmentSmall-scale TVAC chamber for CubeSat testing.
Cleanroom services
ServicesISO Class 7 cleanroom access for satellite integration.
Radiation dosimeters
ComponentsCompact dosimeter sensors for onboard radiation monitoring.
CubeSat deployers
Launch Interfaces12U CubeSat deployer compatible with standard launch vehicles.
S-band transceiver
CommunicationsLooking for S-band transceiver capable of 10 Mbps data rate for LEO satellite constellation.
Solar panel arrays
Power SystemsHigh-efficiency solar panels for small satellite missions, minimum 200W output.
Attitude control thrusters
PropulsionCold gas thrusters for 3U CubeSat attitude control, 1N thrust capability.
Star tracker sensors
NavigationHigh-precision star tracker for deep space navigation, 0.1 arcsecond accuracy.
Thermal control systems
Thermal ManagementPassive thermal control coatings for Mars orbiter mission.
Data storage units
Data SystemsRadiation-hardened solid state drives, minimum 1TB capacity.
Antenna deployment mechanisms
Mechanical SystemsReliable deployment system for deployable mesh antennas.
Battery management systems
Power SystemsLithium-ion battery management for long-duration missions.
X-band payload antenna
CommunicationsLooking for X-band high-gain antenna for 1 Gbps downlink from GEO.
Radiation shielding materials
MaterialsLightweight composite shielding for CubeSats operating in MEO.
Onboard computer (OBC)
Data SystemsFault-tolerant OBC with ARM processor and at least 2GB RAM.
Deployable solar wings
Power SystemsCompact solar wing array with >30% efficiency for microsatellite bus.
Reaction wheels
Attitude ControlSmall reaction wheel assembly for CubeSats, torque up to 0.005 Nm.
Chemical propulsion system
PropulsionMiniature monopropellant system providing 5N thrust for orbital maneuvers.
Deployable drag sails
Deorbit SystemsEnd-of-life deorbit drag sail for 6U CubeSat compliance.
High-speed SDR
CommunicationsSoftware-defined radio capable of Ka-band uplink and downlink.
Sun sensors
NavigationCoarse sun sensors for CubeSat ACS with <5° accuracy.
Li-ion batteries
Power SystemsSpace-qualified 20Ah lithium-ion battery pack for LEO missions.
Deployable booms
StructuresLightweight composite booms for magnetometer deployment.
Cryocoolers
Thermal ManagementMiniature cryocooler for IR detector cooling to 80K.
GNSS receivers
NavigationMulti-constellation GNSS receiver for LEO, timing accuracy <20ns.
Plasma thrusters
PropulsionHall-effect thruster suitable for 200kg spacecraft, Isp > 1500s.
Magnetorquers
Attitude ControlThree-axis magnetorquer rods for CubeSat detumbling.
High-gain parabolic antennas
CommunicationsDeployable reflector antenna for Ka-band comms.
Power distribution unit
Power SystemsRadiation-tolerant PDU for small satellite buses.
Optical communications terminals
CommunicationsLasercom terminal for LEO-to-ground 1 Gbps data rate.
Thermal straps
Thermal ManagementFlexible graphite thermal straps for heat transfer from payload to radiator.
CubeSat structures
StructuresStandardized 12U structure compatible with CubeSat deployers.
Earth observation cameras
PayloadsHigh-resolution imager with 1m GSD for EO missions.
Deployable landing legs
Mechanical SystemsCompact shock-absorbing legs for lunar micro-lander.
Onboard AI processors
Data SystemsRadiation-tolerant AI/ML edge computing module for EO image processing.
ISL terminals
CommunicationsInter-satellite link laser terminal with >1000 km range.
Propellant tanks
PropulsionLightweight composite propellant tanks for 10 bar pressure rating.
Ground station antennas
Ground SystemsPortable S/X-band ground station dish for field deployments.
Deployable reflectors
PayloadsLarge deployable reflector for synthetic aperture radar (SAR).
Flight software
SoftwareAutonomous flight software for CubeSat bus, modular architecture.
Radiators
Thermal ManagementLightweight deployable radiators for LEO spacecraft thermal control.
Space-rated connectors
ComponentsMicro-D connectors rated for vacuum and radiation.
Docking mechanisms
Mechanical SystemsSmall sat docking adapter for on-orbit servicing.
Launch adapters
StructuresMulti-satellite launch adapter for rideshare missions.
Space tethers
Deorbit SystemsElectrodynamic tether for deorbit applications.
Radiation-hardened processors
Data SystemsQuad-core processor hardened for GEO mission lifetimes.
Optical sensors
PayloadsWide-angle optical payload for SSA applications.
RF switches
CommunicationsHigh-power RF switches for satellite communication payloads.
Vibration isolation systems
Mechanical SystemsPassive isolation mounts for optical payload stability.
Deployable antennas
CommunicationsTape-spring antenna for UHF CubeSat communications.
Thermal vacuum chambers
Test EquipmentSmall-scale TVAC chamber for CubeSat testing.
Cleanroom services
ServicesISO Class 7 cleanroom access for satellite integration.
Radiation dosimeters
ComponentsCompact dosimeter sensors for onboard radiation monitoring.
CubeSat deployers
Launch Interfaces12U CubeSat deployer compatible with standard launch vehicles.
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Average number of leads received per month (usually 0-50)
Percentage of leads that converted to a sale/contract
Average revenue per sale/contract
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Monthly revenue (avg)
$26,500
Annual revenue (avg)
$318,000
Standard
Gain$149/month
ROI %
175%
Net gain/year
$313,212
Breakeven leads/mo
1 leads
Premium
Gain$399/month
ROI %
66%
Net gain/year
$316,212
Breakeven leads/mo
1 leads
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