Welcome guest
Flywheel energy storage for spacecraft
Renuganth Varatharajoo, Mohamad Tarmizi Ahmad
Aircraft Engineering and Aerospace Technology
2004
384 - 390
0002-2667
10.1108/00022660410545492
Emerald Group Publishing Limited
Existing customers:
Please login above.
You do not have rights to view the article
Purchase this document:
Price payable:
GBP £13.00
plus handling charge of GBP £1.50
and VAT where applicable.
Purchase
Request this document:
Print or e-mail a document request to your librarian.
Request
Reprints & permissions:
Request
Flywheels can serve not only as attitude control devices, but also as energy storage devices, thereby eliminating the need for conventional batteries. Hence, a combined energy and attitude control system (CEACS) consisting of a double counter rotating flywheel assembly is proposed for small satellites in this paper. The energy level in CEACS depends mainly on the flywheels' speeds. Therefore, a specific flywheel energy management strategy has to be implemented to take into account the limitations of the flywheels, which has not been established until today.
Energy management, Spacecraft, Strategic planning
Research paper