Space Hardware Marketplace

PMD Tanks (Propellant Management Device Tanks)

• 80213-1Total Volume: 1,232 in³ / 20.2 l; Diameter: 13.33 in ID (339 mm ID); Weight: 4.00 lbm (1.8 kg); Operating Pressure: 310 psig (21.4 bar); Propellant Capacity: —; Program: CLASSIFIED; Note: C, 80213 Qualified Environments
• 80277-1Total Volume: 18,450 in³ / 302.5 l; Diameter: 32.84 in ID (834 mm ID); Weight: 32.60 lbm (14.8 kg); Operating Pressure: 250 psig (17.2 bar); Propellant Capacity: 894 lbm NTO (405.5 kg); Program: INSAT; Note: C, 80277 Qualified Environments
• 80296-1Total Volume: 3,575 in³ / 58.6 l; Diameter: 19.03 in ID (483 mm ID); Weight: 8.00 lbm (3.63 kg); Operating Pressure: 425 psig (29.3 bar); Propellant Capacity: —; Program: RCA Sat COM; Note: 80296 Qualified Environments

A family of qualified/flight-proven propellant management device (PMD) tanks from Northrop Grumman, used to store and deliver fuel…

Terran 1

Relativity Space's debut orbital launch vehicle — the world's first 3D-printed rocket — retired after its inaugural flight…

H-IIB

Japan's retired heavy-lift launch vehicle used exclusively to launch the HTV (Kōnotori) cargo spacecraft to the ISS, with…

ATMS Advanced Technology Microwave Sounder

• TypePassive microwave sounder
• Channels22 channels
• Frequency range23 GHz to 183 GHz

Cross-track scanning passive microwave sounder providing atmospheric temperature and moisture profiles for NOAA/NASA weather satellites.

SP1Z

The SP1Z is a solar panel designed for CubeSat structures (1U/2U/3U/4U) featuring high-efficiency triple junction UTJ solar cells…

PICO-SAT

• TypeNanosatellite / CubeSat
• DeveloperWroclaw University of Science and Technology
• MissionTechnology demonstration and space education

PICO-SAT is a nanosatellite research project at Wroclaw University of Science and Technology, exploring small satellite design and…

LISA Pathfinder First Flight Electrospray Thruster

Busek delivered eight electrospray thruster clusters for the NASA/ESA LISA Pathfinder mission, ST7, a technology demonstration mission to…

Custom Hardware and Software Development

• Mechanical development scope1-16U CubeSats: design, verification, analysis, qualification, acceptance
• Electronic development scopeBreadboard development, architecture design, flight/qualification model development, MGSE/EGSE manufacturing, TID verification
• Software development scopeGround and space segment software, flight software, subsystem and payload software (VZLUSAT group tools)

Custom mechanical, electronic, and software development for 1-16U CubeSats, from breadboard to flight qualification.

Space Solar Solutions

• Solar cell efficiencyUp to 34%
• Standard cell areaUp to 81.5 cm²
• Flight-proven solar cell technologiesTriple-junction (ZTJ, ZTJ+ & ZTJ-Ω), Quad-junction (Z4J & Z4J+), Five-junction (IMM-β)

Rocket Lab's Space Solar Solutions offer high-efficiency, radiation-hardened solar cells and customizable solar panel arrays to power spacecraft…

TILT

• Integrate cubesats of sizes from6-16 U
• Axes controlled rotation2 axis
• TRL level9+

TILT is a two-axis rotation integration stand designed for CubeSats ranging from 6U to 16U, facilitating assembly, integration,…

Next Generation On Board Computer (OBC NG)

• Core ASICRadiation-hardened CREOLE chip developed by Beyond Gravity
• ProcessorFault-tolerant SPARC V8
• Integrated functionsCommunication functions, reconfiguration function, mass memory controller, extension possibilities

Radiation-hardened satellite on-board computer built around the Beyond Gravity CREOLE chip with fault-tolerant SPARC V8 processor.

TM/TC Front-End

• Form factor19" 3U hardware platform
• Baseband interfaces60x RS422/LVDS pairs
• IsolationGalvanically isolated, FMEA compliant

Telemetry and telecommand unit for direct spacecraft control during AIT and launch phases — 60x RS422/LVDS pairs, galvanically…

Light-Class Lunar Lander

• Payload capacity to lunar surface50 kg
• Propulsion engineRD840
• PropellantsNT + UDMH

The Light-Class Lunar Lander is a conceptual lunar surface delivery vehicle developed by Yuzhnoye SDO, capable of delivering…

Standard Fluxgate Magnetometer

• Sensor typeTri-axial fluxgate, single or dual sensor configuration
• Noise level< 15 pT/sqrt(Hz) @ 1 Hz
• Long-term stabilityOffset drift < 3 nT/year

Configurable industrial-grade tri-axial fluxgate magnetometer for terrestrial geophysical and field survey applications.

CASPEX 4Mpx Space Camera Head

Space-qualified 4-megapixel CMOS camera head with FPGA-based reconfigurable architecture, global shutter, 2048×2048 resolution, and SpaceWire interface in a…

Water Cooled Baffle

The Water Cooled Baffle is a high vacuum diffusion pump baffle designed by Applied Ion Systems.

NanoCom GS2000

The NanoCom GS2000 is an S-band ground station radio designed to increase data rates between nanosatellites and ground…

Solar Panels for Small Satellites

Deployable and body mounted tailor-made solar array solutions for small satellites, manufactured on PCBs or honeycomb aluminium substrates…