Lockheed CL-475
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Lockheed CL-475 (pendaftaran N6940C)[1] adalah helikopter ringan eksperimental dua-kursi, bermesin tunggal, yang dikembangkan oleh Lockheed untuk mengeksplorasi teknologi rotor rigid (kaku).
CL-475 memiliki rotor utama berbilah tiga dan rotor ekor berbilah dua. Hanya satu dibangun.
Referensi
- ^ Francillon 1987
Wikimedia Commons memiliki media mengenai Lockheed CL-475.
- Francillon, René J. (1982). :Lockheed Aircraft since 1913. London: Putnam & Company. ISBN 0-370-30329-6.
- Francillon, René J. Lockheed Aircraft Since 1913. Annapolis, Md: Naval Institute Press, 1987. ISBN 978-0-85177-805-1
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