Space Hardware Marketplace

Phoenix Eye SignalPrint

• CapabilityUnique RF transmitter fingerprinting / identification
• Use caseDetect spoofed/cloned transmitters despite identical hardware and crypto
• Software typeProprietary COTS DSP software

RF transmitter fingerprinting software that uniquely identifies individual radios even when hardware, firmware and crypto are identical.

Phoenix Eye SyncWave

• Grating lobe removalContinuous elimination of carrier phase differences on baseband data
• Signal source compatibilityAny digitized signal with synchronized sampling clocks (dishes, arrays)
• Input channelsUnlimited (limited by computing capability)

DSP software that removes grating lobes from electronically scanned antenna receivers, enabling coherent combination of any digitized signal.

Cowbell Suborbital Test Rocket

• Length12 meters
• Target test altitude~21,000 meters (suborbital)
• PropulsionRocketStar Aerospike Engine

12-meter aerospike-powered developmental suborbital test rocket intended to fly from Cape Canaveral's Launch Complex 48.

RocketStar Aerospike Engine

• Thrust gain vs. bell-cone25-35% more thrust, no extra fuel
• Performance gain~20% better than conventional rocket engines
• Thrust vectoringIndividually controlled combustion chambers; no gimbals/actuators needed

Patent-pending 3D-printed aerospike rocket engine producing 25-35% more thrust than conventional bell-cone engines with built-in thrust vectoring.

FireStar Fusion Drive

• Base thrusterFireStar Foundation Drive (water-fueled pulsed plasma)
• Fusion fuel additiveBoron (aneutronic fusion in exhaust)
• Thrust improvement~50% higher than FireStar Foundation Drive

Fusion-enhanced evolution of the FireStar water-fueled pulsed plasma thruster, delivering roughly 50% more thrust via aneutronic boron fusion.

FireStar Foundation Drive

Water-fueled pulsed plasma electric thruster in a 1U form factor for smallsat orbit raising, phasing, de-orbit and attitude…

SALSAT

• Type3U CubeSat
• Launch year2020
• Mass~3 kg

SALSAT (Spectrum Analyzer for Low Frequencies at Low Altitudes) is a 3U CubeSat developed by TU Braunschweig, launched…

ROBUSTA-1A

• Type1U CubeSat
• Launch year2012
• Mass~1 kg

ROBUSTA-1A (Radiation On Bipolar University Satellite Test Application) is a 1U CubeSat developed by Club CubeSat at ISAE-SUPAERO…

TUDSaT

• Type1U CubeSat
• UniversityTU Darmstadt
• CountryGermany

TUDSaT is the CubeSat research platform developed by TU Darmstadt students, focusing on satellite bus design, ADCS, and…

TechnoSat

• Type3U CubeSat
• Launch year2017
• OrbitLEO 500 km SSO

TechnoSat is a 3U CubeSat developed by TU Berlin, launched in 2017, designed to test novel satellite bus…

MOVE-II

• Type2U CubeSat
• Launch year2018
• Mass2.4 kg

MOVE-II (Munich Orbital Verification Experiment) is a 2U CubeSat developed by TU Munich students under WARR space group,…

BEESAT-2

• Type1U CubeSat
• Launch year2013
• Mass~1 kg

BEESAT-2 is a 1U CubeSat developed by TU Berlin as a follow-up to BEESAT-1, carrying an improved attitude…

BEESAT-1

• Type1U CubeSat
• Launch year2009
• Mass~1 kg

BEESAT-1 is a 1U pico-satellite developed by TU Berlin students, launched in 2009 as one of Germany’s earliest…

ISTSat-1

ISTSat-1 is Portugal first CubeSat, developed by students at Instituto Superior Tecnico and launched aboard the Vega-C rocket…

Space Physics and Astrophysics Research

• InstitutionAl-Farabi Kazakh National University, Almaty
• Founded1934
• Research AreasAstrophysics, space physics, satellite remote sensing

Al-Farabi Kazakh National University conducts research in space physics, astrophysics, and satellite remote sensing through its Faculty of…

DUTHSat

• TypeCubeSat nanosatellite
• InstitutionDemocritus University of Thrace
• CountryGreece

DUTHSat is a student-built nanosatellite from Democritus University of Thrace, part of Greeces university space program for developing…

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…

HUMSAT-D Educational CubeSat

• Type1U CubeSat
• Form Factor10 x 10 x 10 cm
• Mass≤1.33 kg

1U CubeSat developed by the University of Vigo as a technology demonstrator for the HUMSAT humanitarian communication constellation,…