Space Hardware Marketplace

Green mono-propellant Micro Propulsion System (MiPS)

The VACCO Green MiPS is a self-contained 3U mono-propellant propulsion system for CubeSats, featuring four 100 mN thrusters…

Electronic Design Services

• PCB substrate typesFR4, IMS, flexible, rigid-flex
• Assembly methodsThrough-hole and surface-mount, selective and reflow soldering
• Design capabilitiesAnalog, mixed-signal, digital, RF, high-frequency, power electronics

ALTER Technology provides comprehensive electronic design services from concept to manufacturing, including PCB design (FR4, IMS, flex), FPGA…

DC Block, 1.85mm-m, DC-65GHz (Item #6546-6010-65)

A 1.85mm male-to-female DC block passive microwave component rated from DC to 65 GHz, used to block DC…

CUBESAT TEST POD

A secure test pod designed for environmental testing of CubeSats ranging from 6U to 16U, facilitating easy and…

Multi-Purpose Interface Platform (MPIP)

Modular, scalable EGSE testing spacecraft electrical/data interfaces — supports up to 16 modules, >400 channels, ESA/ECSS compliant.

Reuse launch vehicle

The reuse launch vehicle aims to reduce waste and lower production and launch costs by enabling multiple uses…

Y50DX series

• StandardGJB101A-97
• Couplingbayonet

The Y50DX series circular electrical connector conforms to Chinese military connector standard GJB101A-97, offering bayonet coupling, small volume,…

Azista BST Aerospace Satellite Manufacturing Services

Azista BST Aerospace is a vertically integrated satellite manufacturing company offering end-to-end solutions for small satellites (50-200kg) and…

Xidus-Studio

• GNSS SystemsGPS, GLONASS, GALILEO, BEIDOU
• Augmentation SystemsWAAS, MSAS, EGNOS, GAGAN, SDCM
• Platform SupportWindows, Linux

Xidus-Studio is a powerful configurator and viewer client software for the Xidus GNSS simulator, offering flexibility and unique…

H2O2/HTPB Hybrid Upper Stage

• PropellantsH2O2 (hydrogen peroxide) / HTPB
• ApplicationSmall launch vehicle upper stage
• IgnitionCustom pyrotechnic or spark ignition hardware

High-performance hydrogen peroxide / HTPB fueled hybrid rocket upper stage for small launch vehicles.

Attitude Control Module PnP ADCS-N1

• Star tracker - quantity2
• Star tracker - accuracy (Pointing/Rolling)5" (3sigma) / 50" (3sigma)
• Star tracker - update rate10 Hz

A plug-and-play (PnP) satellite attitude determination and control module (ADCS-N1) integrating star trackers, sun sensor, gyroscope, magnetometer, reaction…

1.0m X-band portable station

A 1.0m X-band portable ground station for rapid deployment, enabling telemetry, tracking, and command (TT&C) operations with LEO…

Attitude Determination and Control System (ADACS) Kit

The Attitude Determination and Control System (ADACS) Kit provides a comprehensive solution for spacecraft attitude control.

NEPTUNE_100 Launch Vehicle

• Vehicle classSmall-lift orbital
• Stages2
• Payload to 500 km polar orbit100 kg

Low-cost small-lift two-stage orbital rocket delivering 100 kg to 500-km polar orbit at $599,999 per dedicated launch.

Grad-13®

• Baselines500 mm to 1000 mm
• VersionsLand and submersible (200m)
• Measuring range±70 or ±100μT

The Grad-13 is a digital three-axis gradiometer providing high resolution vector measurements of magnetic fields on land or…

Lighting Vision System

The Kayser Lighting Vision System provides stable and reliable illumination for in-orbit servicing, robotic operations, and inspection activities…

PocketQube Satellite Structure

• Form factors1P, 2P, 3P PocketQube
• Compatible deployerMR-FOD
• Launch platformItalian UniSat micro-satellite

Standard PocketQube satellite structures in 1P, 2P, and 3P sizes for launch via the MR-FOD deployer.

Satellite Qualification & Acceptance Testing Services

Full-spectrum spacecraft environmental qualification and acceptance testing: vibration, shock, thermal-vacuum, and cleanroom services.