Features inherent in designing MI-60 MAI superlight helicopter powered by two piston engines
Features inherent in designing MI-60 MAI superlight helicopter powered by two piston engines
| dc.contributor.author | Tischenko, M.N. | |
| dc.contributor.author | Ivtchin, V.A. | |
| dc.contributor.author | Artamonov, B.L. | |
| dc.date.accessioned | 2016-06-30T11:50:03Z | |
| dc.date.available | 2016-06-30T11:50:03Z | |
| dc.date.issued | 2000 | |
| dc.identifier.other | 06_11 | |
| dc.identifier.uri | http://hdl.handle.net/20.500.11881/505 | |
| dc.language.iso | en | |
| dc.subject.other | Rotorcraft design | |
| dc.title | Features inherent in designing MI-60 MAI superlight helicopter powered by two piston engines |
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