NASA NTRS · 19790015748
Overview of helicopter ice protection system developments
Abstract
Helicopter ice protection design criteria was developed and technological shortcoming in meeting helicopter mission requirements is that of helicopter rotor blade ice protection. Airframe components are protected using existing technology while the rotor blade protected using the cyclic electrothermal deicing concept.
Keep this discovery
Explore connections, maps & timelines
Richard I Adams. 1979-01-01. Overview of helicopter ice protection system developments. https://ntrs.nasa.gov/citations/19790015748
Cite the original work for its findings. Save a collection to share your selection of sources.