Grow your business with satsearch

Tap into opportunities to sell to space customers all around the world

Get in touch to join the satsearch trusted supplier network

Used by engineers from:
ST Engineering
Iceye
Reflex Aerospace
Pixxel
ESA
NASA
Northrop Grumman
Kepler Communications
GISTDA
ATMOS Space Cargo
Azista
egSA
Azista
egSA
L3Harris
UAE Space Agency
Exotrail
Link
Fleet
OHB
DLR
Eutelsat
Satellogic
Lockheed Martin
ST Engineering
Iceye
Reflex Aerospace
Pixxel
ESA
NASA
Northrop Grumman
Kepler Communications
GISTDA
ATMOS Space Cargo
Azista
egSA
Azista
egSA
L3Harris
UAE Space Agency
Exotrail
Link
Fleet
OHB
DLR
Eutelsat
Satellogic
Lockheed Martin
Used by engineers from:
ST Engineering
Iceye
Reflex Aerospace
Pixxel
ESA
NASA
Northrop Grumman
Kepler Communications
GISTDA
ATMOS Space Cargo
Azista
egSA
Azista
egSA
L3Harris
UAE Space Agency
Exotrail
Link
Fleet
OHB
DLR
Eutelsat
Satellogic
Lockheed Martin
ST Engineering
Iceye
Reflex Aerospace
Pixxel
ESA
NASA
Northrop Grumman
Kepler Communications
GISTDA
ATMOS Space Cargo
Azista
egSA
Azista
egSA
L3Harris
UAE Space Agency
Exotrail
Link
Fleet
OHB
DLR
Eutelsat
Satellogic
Lockheed Martin

more than 25,000 space
engineers

use satsearch
every month

400+
$1B+
10,000+

Browse the latest capabilities that qualified buyers
are looking for on satsearch right now

Open
PAYLOAD PROCESSOR

We are a graduate research team in South Korea, developing
a 6U CubeSat for an advanced-track CubeSat competition. We are looking for an
ONBOARD AI PAYLOAD PROCESSOR and would like to gather options and approximate
pricing from multiple suppliers.

Mission summary:
- 6U CubeSat, LEO (~500–600 km)
- Primary mission: optical observation of resident space objects / debris
- Imaging triggered by TLE predictions (event-based capture, no active tracking)
- Onboard AI task: detection + coarse classification of space objects from
captured monochrome images (batch / event-based inference, NOT continuous
real-time processing — so heavy compute is not required)

Requirements / preferences for the AI processor:
- CubeSat-compatible form factor, within ~1U, low power (6U power budget)
- Capable of running a lightweight CNN for detection + coarse classification
- Data interface able to receive images from a monochrome CMOS camera
- Radiation mitigation suitable for a short LEO mission
- LOW COST is a priority — please indicate the most budget-friendly option
and any academic / research / student-competition discount
- Engineering model (EM) availability for ground testing is a plus

For each suggested product, we would like:
1. Approximate unit price (+ academic/research discount if any)
2. Lead time
3. AI performance (TOPS), power consumption, size, mass, interfaces
4. Flight heritage / TRL and radiation-mitigation approach
5. Export-control status for shipping to South Korea

Expected timeline: [launch around 2027 /delivery date]. Quantity: [e.g. 1 EM + 1 FM]

Submit your bid
Open
Reaction wheels

RFQ for Reaction wheels with at least 4Nms momentum storage and max torque of at least 250 mNm

Submit your bid
Open
Ka-band transceiver + antenna

RFQ for a Ka-band transceiver + antenna

Submit your bid
Open
Solar Cells
CategoryParameterMission RequirementExpected Unit / FormatNotes & Testing Conditions
VolumeNumber of units20-50pcsPossibility to scale up if price is good
Electrical (AM0)BOL Efficiency≥ 28% (ideally 29–30%%Measured at AM0, 28°C
 EOL Efficiency≥ 24% after mission%At mission-specific radiation dose
 Max Power Voltage (Vmp​)≥ 2.2 VVMeasured at AM0, 28°C
 Max Power Current (Imp​)As high as possiblemA/cm² or AMeasured at AM0, 28°C
 Open-Circuit Voltage (Voc​)≥ 2.5 VVMeasured at AM0, 28°C
 Short-Circuit Current (Isc​)As high as possiblemA/cm² or AMeasured at AM0, 28°C
MechanicalCell ArchitectureTriple Junction (GaInP/GaAs/Ge) or high-end IBC Mono SiTexte.g., 3J (InGaP/InGaAs/Ge)
 Cell Dimensions40 × 80 mm (±0.5 mm) or similarmm x mmWidth x Length
CIC AssemblyCoverglass Thickness100 – 300 µmµm or mils 
 Coverglass CoatingsAR + UV RejectionTexte.g., AR, UV Rejection
 Interconnect DesignStandard with stress reliefTextMaterial and stress relief type
 Bypass Diode TypeExternal Si diodeTextMonolithic or Discrete
 Contact LayoutFront-to-Back or All-BackTexte.g., Front-to-Back, All-Back
Heritage & QAFlight HeritageLEO preferredOrbit / Mission ListProven in LEO/MEO/GEO?
 Space Standard Auth.ECSS or equivalentTexte.g., ECSS, AIAA
 LAT DocumentationYesYes/NoLot Acceptance Test reports
Submit your bid
Open
Satellite Educational Kits

1. Educational Satellite Development Kit
• For teaching spacecraft subsystems, embedded systems, communications, power management, and mission operations Qty: 1
2. Single Axis Reaction Wheel Module
• For attitude determination and control experiments
• Compatible with educational satellite platforms Qty: 1
3. Satellite Test Bench – FlatSat Configuration
• Hardware in the loop (HIL) test bench
• For subsystem integration, verification, validation, and FlatSat testing Qty: 1
4. 2U Satellite Structure Expansion Kit
• Modular structure for additional payloads and subsystems Qty: 1
5. Satellite Storage & Transport Case
• Protective case for satellite hardware and accessories Qty: 1
6. Motor Control Development Kit (Dual DC Motors)
• Controls two DC motors
• Uses external power source Qty: 1
7. Microcontroller Based Motor Control Development Kit
• Python programmable
• Wireless IoT connectivity
• Embedded control applications Qty: 1
8. Dual Axis Robotics Educational Kit
• Wireless communication
• 9 DOF IMU
• Ultrasonic distance sensor
• Programmable microcontroller Qty: 2
9. Python Programmable Microcontroller Educational Kit
• Wireless IoT connectivity
• Ultrasonic distance sensor
• Infrared sensing modules
• Plug in expansion capability Qty: 2

Submit your bid
Open
Battery
CategoryParameter NameTarget ValueUnit
Programmatic1. Quantity & Schedule1FM asap (<1 Month)Qty / Date
Electrical2. Nominal Voltage5V,12VV
3. Total Energy Capacity100Wh
4. Max Continuous Current5A
5. Peak Current & Duration7A for 200msA / ms
Mechanical6. Maximum Mass1.4kg
7. Max Envelope (X x Y x Z)100x100x200mm
Environmental8. Operational Temp Range-45to +65°C
9. Launch Vibration (Random)5.57g rms
Mission Life10. Orbit Type & Design LifeLEO, 2 YearsOrbit / Yrs
11. Max Depth of Discharge30%
Quality12. Mission Class / StandardSpace qualified TRL9 
Submit your bid
Open
Solar Cell

We need a small solar cell for a distributed lunar science mission. Final mission may need 50-150 of the cells, however we want to understand the pricing and availability of 3J or 4J cells to test and integrate before possible launch. We aim for smaller than 70mm max length, however we may go with an 80 mm by x mm model if needed.
 

Submit your bid
Open
Thermal shock test services

Provision of thermal shock test services (Two-zone elevator thermal shock chamber):
-Device under test:
-6 units of sandwich panels (35 x 16cm x 2cm)
-Test conditions:
-Hot temperature: +115 deg (+-5deg)
-Cold temperature: -110 deg (+-5deg) (flexible, -70deg is the minimum requirement)
-1 min dwell time
-Test cycles:
-Total 30k
-Inspection points:
-One visual inspection after 5k cycles since start
-One visual inspection after 15k cycles since start
-One visual inspection after 30k cycles since start
Expected response to the tender
-Response deadline: 20/07/2026
-Response content:
-FFP price for the mentioned campaign
-If applicable, 2 prices can be quoted, one for the -110 deg temp and another for the -70 deg temp
-Proposed schedule
-Including, at least, 2 days window for a 4h visual inspection
-Thermal shock chamber technical description
-Accommodation of the DUTs (Device Under Test)

Submit your bid
Open
Lightweight cryogenic pressure vessel / bottle for gaseous helium

We are seeking a quotation for a lightweight cryogenic pressure vessel / bottle for gaseous helium service. Please review the requirements below and confirm your capability to supply or fabricate a suitable vessel.
Technical requirements
- Minimum internal volume: approximately 30 litres
- Maximum outer radius: approximately 0.30 m
- Maximum expected operating pressure: approximately 300 bar
- Service: gaseous helium
- Exposure: liquid oxygen
- Cryogenic compatibility over temperature range: 90 K to 330 K
- Preference: minimum mass, subject to safe design, qualification, and compliance requirements

Submit your bid
Open
S-band transceiver

We are looking for suitable S-band transceiver/transponder options for a CubeSat communication subsystem.

The unit should be suitable for a CubeSat mission and support S-band communication with two wideband full-duplex S-band antennas. We are exploring an antenna-selection architecture where the communication subsystem can select the antenna with better received-link quality during operation.
S-band uplink and downlink capability suitable for CubeSat TT&C / data communication.
Full-duplex operation preferred, or clear details on supported half-duplex/full-duplex modes.
Compatibility with two wideband S-band antennas.
Support for single-antenna and/or dual-antenna configuration.
Ability to support antenna selection using either:
1. internal RF switching,
2. transceiver-controlled external RF switch,
3. configurable GPIO / antenna-select output, or
4. OBC-controlled external RF switch.
Ability for the OBC to read RX QoS metrics and command antenna selection, if supported.
Clear RF interface information:
1. single common RF antenna port or separate TX/RX RF ports,
2. RF connector type,
3. output power,
4. receiver sensitivity,
5. required duplexer/diplexer/filtering, if any.

OBC interface details: UART, SPI, CAN, RS-422, RS-485, or other supported digital interface,

Flight heritage, qualification status, environmental test levels, and radiation information.
Availability of engineering model, qualification model, and flight model units.
Current lead time, approximate cost, and procurement options.
Datasheet, ICD, user manual, and application notes. If detailed documents require NDA, please mention the process.


We are currently performing a high-level trade study and would like suppliers to recommend suitable products or configurations, including any required external hardware such as RF switch, duplexer/diplexer, filters, power amplifier, or interface boards.

Submit your bid

Curious to learn more?

satsearch COO Narayan explains it all

Ready to hop on board?
Join dozens of Trusted Suppliers

2NDSpace
AAC Clyde Space
Accord Software & Systems Private Limited
ACM Coatings GmbH (subsidiary of Acktar Ltd.)
Alén Space
ANT61
Anywaves
arcsec
Auria
Av-Comm Space and Defence
Azista
Bradford Space
Colossus
cosine Remote Sensing B.V.
Cosmic Shielding Corporation
CUBECOM
CubeSpace
Dhruva Space
Dragonfly Aerospace
ECAPS
EDGX
Electronic Communication Systems FZC
EnduroSat
EOSOL Aerospace
Epsilon3
EXA (Ecuadorian Space Agency)
Exobotics
Global Commutech PTE. LTD.
HEX20 Labs India Private Limited
Ibeos
IENAI SPACE
Infinity Avionics Pty Ltd
INVENT GmbH
IQ spacecom
Kongsberg NanoAvionics
LANTIAN SOLAR
LANZO Batteries
Leaf Space
Liftero
Lightfoundry
Manastu Space Technologies
MVP Aerospace Ltd
Needronix
NewSpace Systems
Novo Space
NPC SPACEMIND
Omnetics Connector Corp.
Oxford Space Systems
Paradigma Technologies
PICOSATS SRL
PlaneWave Inc.
Printech Circuit Laboratories Ltd
Rafael Ltd.
ReliaSat
Remos Space Systems AB
Resonate Testing Ltd
Satlab A/S
SATLANTIS
Scanway S.A.
Simera Sense
SkyFox Labs s.r.o.
SkyLabs d.o.o.
Sodern S.A.
Solar MEMS Technologies S.L.
Spacebackend
Space Inventor
SPACERACE
SteamJet Space Systems
TakeMe2Space
Tensor Tech
Terma
TRL Space
Unibap Space Solutions AB
VEOWARE SPACE
Xiphos
Zero-G Radiation Assurance
Zoppas Industries Heating Element Technologies - IRCA SPA
2NDSpace
AAC Clyde Space
Accord Software & Systems Private Limited
ACM Coatings GmbH (subsidiary of Acktar Ltd.)
Alén Space
ANT61
Anywaves
arcsec
Auria
Av-Comm Space and Defence
Azista
Bradford Space
Colossus
cosine Remote Sensing B.V.
Cosmic Shielding Corporation
CUBECOM
CubeSpace
Dhruva Space
Dragonfly Aerospace
ECAPS
EDGX
Electronic Communication Systems FZC
EnduroSat
EOSOL Aerospace
Epsilon3
EXA (Ecuadorian Space Agency)
Exobotics
Global Commutech PTE. LTD.
HEX20 Labs India Private Limited
Ibeos
IENAI SPACE
Infinity Avionics Pty Ltd
INVENT GmbH
IQ spacecom
Kongsberg NanoAvionics
LANTIAN SOLAR
LANZO Batteries
Leaf Space
Liftero
Lightfoundry
Manastu Space Technologies
MVP Aerospace Ltd
Needronix
NewSpace Systems
Novo Space
NPC SPACEMIND
Omnetics Connector Corp.
Oxford Space Systems
Paradigma Technologies
PICOSATS SRL
PlaneWave Inc.
Printech Circuit Laboratories Ltd
Rafael Ltd.
ReliaSat
Remos Space Systems AB
Resonate Testing Ltd
Satlab A/S
SATLANTIS
Scanway S.A.
Simera Sense
SkyFox Labs s.r.o.
SkyLabs d.o.o.
Sodern S.A.
Solar MEMS Technologies S.L.
Spacebackend
Space Inventor
SPACERACE
SteamJet Space Systems
TakeMe2Space
Tensor Tech
Terma
TRL Space
Unibap Space Solutions AB
VEOWARE SPACE
Xiphos
Zero-G Radiation Assurance
Zoppas Industries Heating Element Technologies - IRCA SPA

Thousands of buyers are looking for you,
don't keep them waiting.

Narayan Prasad - Chief Operating Officer

Get started today