The design, manufacture and certification of emergency inflation systems for helicopters

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.69, Iss.3, 1997-06, pp. : 247-253

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Design and Testing of Float Landing Gear Systems for Helicopters

By Alcedo Anthony M.

Journal of the American Helicopter Society, Vol. 25, Iss. 3, 1980-07 ,pp. : 3-9

AHS International

Access to resources Recommend Favorite

FAA Certification of Turbine Transport Helicopters

By Sabo J. A. Dumont T. E.

Journal of the American Helicopter Society, Vol. 7, Iss. 1, 1962-01 ,pp. : 40-51

AHS International

Access to resources Recommend Favorite

Structural Design for Amphibious Helicopters

By Rich Melvin J.

Journal of the American Helicopter Society, Vol. 7, Iss. 3, 1962-07 ,pp. : 17-27

AHS International

Access to resources Recommend Favorite

Acoustic Design for Transport Helicopters

By Sternfeld Harry Miller Laymon N. Beranek Leo L.

Journal of the American Helicopter Society, Vol. 2, Iss. 4, 1957-10 ,pp. : 21-28

AHS International

Access to resources Recommend Favorite

Emergency-Power Benefits to Multi-Engine Helicopters

By Semple R. D. Yost J. H. King E. W. Gonsalves J. E. Thompson W.

Journal of the American Helicopter Society, Vol. 22, Iss. 3, 1977-07 ,pp. : 27-33

AHS International

Access to resources Recommend Favorite