NanoACE Satellite

NanoACE
NanoACE
NanoACE
Name NanoACE
Form factor CubeSat
Units or mass 3U
Status Operational? (Tyvak paper in CubeSat Developers Workshop 2018 but no news since then for the past 5 years, could be retired)
Launched 2017-07-14
NORAD ID 42844
Deployer EXOpod 12U/16U [Exolaunch]
Launcher Sojuz-2-1a
Entity name Tyvak
Institution Company
Entity Commercial
Nation US
Manufacturer AIVT by Terran Orbital
Launch brokerer Exolaunch
Oneliner

Validate CubeSat platform technologies and test propulsion module plus cameras.

Description

Validate the Endeavor suite technologies that will be used for future missions and is solely for the purpose of internal Tyvak development as an attitude control experiment. Includes VACCO propulsion module. Validate the Command and Data Handling (CDH) system, Guidance Navigation and Control (GNC) software and actuators, as well as test visible & IR cameras.

Sources [1] [2]
Photo sources [1]
COTS subsystems
  • PLATFORM - Tyvak
Keywords Propulsion
On the same launch

Last modified: 2024-05-29

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Created by Erik Kulu

Email: erik.kulu@nanosats.eu
LinkedIn: linkedin.com/in/erikkulu

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