µDragonfly Bus

µDragonfly Bus image

Overview

The Dragonfly Aerospace µDragonfly Bus is designed to provide stable and precise Earth-imaging capability across a range of spectra. The system has an automated Attitude and Orbit Control System (AOCS) including a Xenon electric propulsion unit. Communication is enabled via an X-band data downlink and S-band TMTC, and the bus includes various electrical interfaces for simple integration with a range of payloads.


Attitude and Orbit Control
• Pointing Control Stability → <0.0015°/sec (3-sigma)
• Pointing Control Accuracy → <0.01° (3-sigma)
• Slew Rate → Up to 4°/sec


Communications
• S-Band TMTC → 400 kbps down, 150 kbps up

• X-Band Data downlink → 2.5 Gbps (Peak)


Electrical Power System
• Solar Array Peak Power → 220 W
• Orbit Average Power (OAP) → 140 W


Electrical Interfaces
• TMTC → CANbus, RS422/RS485
• Data → LVDS / SpaceWire / SerDes


Payload
• Available Mass → Up to 100 kg
• Available Volume → Ø500 mm x 1000+ mm

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Overview

Name
µDragonfly Bus
Component Type
SmallSat Platform
Form Factor
SmallSat
Heritage
N/A

Details

Class
100 kg
Energy Storage
Up to 600 Wh
Lifetime
5 Years
Payload available mass
Up to 70 kg

Vendor Details

Name
Dragonfly Aerospace
Founded
2020
Summary
Dragonfly Aerospace envisions a future in which our small, high-performance imaging satellites and payloads enable large imaging constellations that provide persistent views of the Earth in a variety of spectrums, providing unprecedented business intelligence and improving people's lives all over the world. Dragonfly Aerospace satellites and payloads are built on a 25-year legacy of components and design principles that date back to the first South African microsatellite, SUNSAT, which was launched in 1999. Since South Africa's entry into the space race, members of our team have worked on every microsatellite space mission.

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Specifications

Component Type
SmallSat Platform
Form Factor
SmallSat
Dry Mass
100.0 kg
Average Power
N/A
Heritage
N/A
Status
In Production
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