Reference number
ISO 21648:2008
International Standard
ISO 21648:2008
Space systems — Flywheel module design and testing
Edition 1
2008-12
Read sample
ISO 21648:2008
46090
Published (Edition 1, 2008)
This publication was last reviewed and confirmed in 2019. Therefore this version remains current.

ISO 21648:2008

ISO 21648:2008
46090
Language
Format
CHF 151
Convert Swiss francs (CHF) to your currency

Abstract

ISO 21648:2008 establishes the design, analysis, material selection and characterization, fabrication, test and inspection of the flywheel module (FM) in a flywheel used for energy storage in space systems. These requirements, when implemented on a flywheel module, will ensure a high level of confidence in achieving safe operation and mission success. With appropriate modifications, ISO 21648:2008 can also be applied to similar devices, such as momentum and reaction wheels and control-moment gyroscopes.

The requirements set forth in ISO 21648:2008 are the minimum requirements for flywheel modules in flywheels used in space flight applications. They are specifically applicable to the parts in the flywheel rotor assembly (FRA), including rim, hub and/or shaft and other associated rotating parts, such as the bearings and the motor generator rotor. The requirements are also relevant to the non-rotating parts, such as module housing, main suspension assembly (magnetic or rolling element bearings, superconductor bearings, etc.), motor stator, caging mechanism and sensors within the module housing, and backup bearings, if applicable. However, control and interface electronics are not covered in ISO 21648:2008.

General information

  •  : Published
     : 2008-12
    : International Standard under systematic review [90.20]
  •  : 1
     : 28
  • ISO/TC 20/SC 14
    49.140 
  • RSS updates

Got a question?

Check out our Help and Support