DODONA
Mission information
Name
DODONA
Satellite ID
FWFR-1086-4147-8825-4245
NORAD ID
51084
Website
https://www.isi.edu/centers-serc/research/nanosatellites/dodona/
Country of Origin

United States of America

Status
Satellite re-entered
Decayed

Satellite has re-entered

Image
DODONA
Mission timeline
Launch Date
2022-01-13T15:25:00+00:00
Deploy Date
2022-01-24T09:02:00+00:00
Decay Date
2024-05-23T00:00:00+00:00
Description

This is the third nanosatellite project for SERC and USC intended to fly new payloads and demonstrate various control and communications techniques. A new B-Dot control algorithm will be demonstrated for optimal stability control with low power using torque rods, a rotating multi-packetized beacon transmission source to prove backup to the primary communications system, and data store and forward software to be demonstrated for non-consistent ground contacts. The Cubesat bus is a MISC-2 variant, a sister of the Aeneas design and will use the same flower petal configuration for primary solar array power.

Mode U - GFSK19k2 AX.25
Type
Transmitter
Downlink Mode
FSK
Downlink Frequency
401500000
Baud
19200
Most Recent Observers (last 24h)

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