Space Hardware Marketplace

Vega C

• Height~35 m
• Liftoff mass~210 tonnes
• Fairing diameter3.3 m

Vega C is Avio's single-body, four-stage small/medium-lift launcher, the upgraded successor to Vega, built for ESA/Arianespace to serve…

Miura 5

• Height35.7 m
• Diameter2 m
• Stages2 stages + optional kick stage

Miura 5 is PLD Space's two-stage, reusable orbital launch vehicle for small satellites, currently in development to offer…

Terran R

• Height284 ft (86.6 m)
• Diameter17.7 ft (5.4 m)
• Payload fairing diameter5 m

Terran R is Relativity Space's next-generation, fully reusable, 3D-printed two-stage rocket designed to serve the growing LEO, MEO,…

Miura 1

• Length12.5 m
• Diameter0.7 m
• Stages1

Miura 1 is PLD Space's single-stage, reusable suborbital sounding rocket that became the first privately developed European rocket…

Alpha

• Overall length29.48 m (96.7 ft)
• Fairing height5 m (16.4 ft)
• Fairing diameter2.2 m (7.2 ft)

Firefly Aerospace's operational two-stage orbital launch vehicle for dedicated small satellites, rideshare payloads, and hypersonic testing.

Hermes In-Space Propulsion Unit

Integrated hydrogen-peroxide monopropellant propulsion unit for small satellite maneuvering.

Aurora

Two-stage hybrid rocket small launch vehicle for dedicated small-satellite missions to LEO/SSO.

Komodo Imager

• Spatial Resolution (GSD) at 500 km — RGB1.5 m
• Spatial Resolution (GSD) at 500 km — MSPAN 1.5 m / MS 3 m (binned 2x2)
• Swath at 500 km6.1 km (RGB), 15 km (MS)

High-performance multispectral CubeSat camera in a compact 12U/16U form (roadmap, TRL 5).

Gecko Imager

Compact RGB imager for CubeSats as small as 1U-2U.

ηDragonfly Bus

• Class50 kg bus, 15" port
• Lifetime5 years
• Energy Storageup to 300 Wh

50 kg nano-class satellite bus leveraging EOSSAT-1 avionics heritage, deployable multiple-per-launch.

Dragonfly Bus

• Class150 kg (up to 400 kg combined bus and payload)
• Lifetime8 years
• Energy Storageup to 2400 Wh

150 kg-class satellite platform for larger, power- and data-intensive Earth observation and SAR missions.

Raptor Imager

• Spatial Resolution (GSD) at 500 kmPAN 0.5 m (native) / 0.36 m (super-resolution) / MS 2 m
• Swath at 500 km8 km
• Mass (incl. electronics)≈ 60 kg

Very-high-resolution panchromatic/multispectral imager for microsatellites (roadmap, TRL 5).

DRAGONEYE

• Spatial Resolution (GSD) at 500 kmPAN 1.4 m, MS Binned 2.8 m
• Swath at 500 km22.2 km
• Mass (incl. electronics)18 kg

Very-high-resolution imager for microsatellites, with flight heritage from 2023.

μDragonfly Bus

• Class100 kg bus
• Lifetime5 years
• Energy Storageup to 600 Wh

100 kg-class microsatellite platform optimised for very-high-resolution Earth observation, flight-proven on EOSSAT-1.

Chameleon Imager

• Spatial Resolution (GSD) at 500 km — RGB10 m
• Spatial Resolution (GSD) at 500 km — MS/HSPAN 10 m, MS 20 m / binned to 20-40 m
• Swath at 500 km39 km (RGB/MS), 20 km (HS)

High-performance hyperspectral CubeSat imager, 2.5U form factor.

Chameleon Swir

• Spatial Resolution (GSD) at 500 kmRAW 8.7 m
• Swath at 500 km11.2 km
• Mass (incl. electronics)1.6 kg

Short-wave infrared imager for CubeSats, 2.5U form factor.

Caiman Imager

• Spatial Resolution (GSD) at 500 km — RGB3.25 m
• Spatial Resolution (GSD) at 500 km — MSPAN 3.25 m; MS 6.5 m
• Swath at 500 km13 km

High-resolution multispectral imager for 6U CubeSats.

Mantis Imager

• Spatial Resolution (GSD) at 500 km — RGB16 m
• Spatial Resolution (GSD) at 500 km — MS/HSPAN 16 m; MS 32 m
• Swath at 500 km32 km

Multispectral/hyperspectral CubeSat imager for platforms as small as 2U.