2550 Crescent Drive, Lafayette, CO 80026 | B L U E C A N Y O N T E C H . C O M

MICROSAT SPACECRAFT

C L A S S24” launch vehicle interface

A V A I L A B L E P A Y L O A D V O L U M E30.0” X 30.0” X 40.0” (typical) Larger volume available within r ideshare envelope and in dedicated launch vehicle fairings

E N E R G Y S T O R A G E40.8 Ah or 54.4 Ah

S O L A R A R R A Y P O W E RHyperion 15, two wing: 1000W Hyperion 15, one wing: 500W

O R B I T A L T I T U D E / O R B I T L I F E T I M ELEO (≥ 5 years), GEO (≥ 2 years), Deep Space (≥ 2 years)

P O I N T I N G A C C U R A C Y±0.002° (1-sigma), 3 axes, 2 Trackers

P A Y L O A D M A S S C A P A B I L I T Y200 kg

X-SAT S A T U R N C L A S S

SPACECRAFT SUMMARY

We are a complete end-to-end spacecraft company and a leading provider of turnkey small satellite solutions, including nanosatellites, CubeSats and Microsats.

Our attitude determination and control components are one-of- a-kind, allowing for industry-leading precision pointing platforms.

X - S A T M E R C U R Y C L A S S

O R B I T A L T I T U D E / O R B I T L I F E T I M E

S O L A R A R R A Y P O W E R

P A Y L O A D V O L U M E

C L A S S

P O I N T I N G A C C U R A C Y

E N E R G Y S T O R A G E

±0.002° (1-sigma), 3 axes, 2 Trackers

X - S A T V E N U S C L A S S

20.5” X 16.4” X 27.0” (1 array)

17.0” X 16.4” X 27.0” (2 array)

Larger volume available depending on launch

vehicle

THEA, two wing: 384WTHEA, one wing: 192W

X - S A T S A T U R N C L A S S

Hyperion 15, two wing: 1000WHyperion 15, one wing: 500W

24” launch vehicle interface8” launch vehicle interface (optional 11.32” available)

15” launch vehicle interface

LEO (≥ 5 years), GEO (≥ 2 years), Deep Space (≥ 2 years)

14.0” X 17.0” X 17.0” (launch dependent)

48W/wing,98W max

30.0” X 30.0” X 40.0” (typical)

Larger volume avail-able within r ideshare envelope and in ded-icated launch vehicle

fair ings

10.2 Ah 10.2 Ah 40.8 Ah or 54.4 Ah