Launch Vehicles — Space Hardware Marketplace

Dauntless

• Height35 m (~115 ft)
• Stage 1 diameter2.5 m (~8 ft)
• Stage 2 diameter2.15 m (~7 ft)

Two-stage small-satellite launch vehicle powered by Vaya Space's vortex-hybrid STAR-3D engines.

Skyrora XL

Three-stage small satellite orbital launch vehicle targeting Sun-Synchronous and Polar orbits.

Bloostar

Balloon-launched orbital rocket; 75 kg to 600 km SSO, methane/LOX propulsion.

HyperSat Satellite Platform — Polish Space Electronics and Nanosatellite Systems

Creotech Instruments S.A. is a Polish space electronics company founded in 2010 in Piaseczno (near Warsaw), designing and…

Ariane 5 / Ariane 6 Structural Components and VESPA Satellite Adapter

Beyond Gravity (formerly RUAG Space) is a Swiss-Swedish space technology company providing structural components, avionics, and satellite dispenser…

M-10 / DM-1650 Solid Rocket Booster Motors for Ariane 5 and Ariane 6

Nammo (Nordic Ammunition Group) is a Norwegian-Finnish defense and aerospace company headquartered in Raufoss, Norway, specializing in solid…

Angular accelerometer

The accelerometer provides measurement of the apparent acceleration of ballistic and space equipment.

String accelerometer

The accelerometer provides measurement of the apparent acceleration of ballistic and space equipment.

Dynamic Pressure Sensor Vt 206

Version: strain gauge sensor with cable jumper. Upon customer's request, it is made with a screwed fitting and…

Pressure Sensor DAV 067

Exception: the strain gage sensor can be supplied with a shock absorber at the request of the consumer.…

Pressure Sensor DAV 068

It is made according to "Regulation 98". Execution: the strain gage sensor at the request of the consumer…

Transition Compartment

Flight-proven transition/adapter compartments for Soyuz (Ø3715/4110 mm) and Zenit (Ø4100 mm) launch vehicles (345–465 kg) for spacecraft-LV interface.

Asynchronous controlled electric motor

The asynchronous controlled electric motor has a 2-phase supply voltage of 40 V, 1000 Hz; the speed of…

Thermoelectric Converter DT 27

Version: thermoelectric converter (TC) consists of a sensitive element placed in the housing, a cable jumper and a…

DHS 514 Pressure Converter

It is made according to "Regulation 88". Version: piezoelectric transducer, consisting of a sensitive element installed in the…

DHS 517 Pressure Converter

It is made according to the "Regulation 98". Version: piezoelectric transducer, consisting of a sensor installed in the…

Fairing

Flight-proven head fairings for Soyuz (Ø3715 mm) and Zenit (Ø4100 mm) launch vehicles (1180–1870 kg) for spacecraft aerodynamic/thermal…

Sensor of a Difference of Pressure DRI 095

Version: monoblock, including a primary inductive converter and a gain unit. The sensor is tight. Permissible leakage is…