Landing gear design challenges for V/STOL service are identified as imposed by weight, ground flotation, rough field operation, drift landings and takeoffs, landing load factor, cost, maintainability, and reliability; general approach, taken by LTV Aerospace Corp, to design of XC-142A, V/STOL transport, landing gear system is described; design of nose gear presented unusually complex requirements which are indicated.
Challenges in landing gear design for V/STOL service XC-142a
SAE -- Paper
SAE Meeting ; 1965
1965
10 pages
Aufsatz (Konferenz)
Englisch
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Challenges in Landing Gear Design for V/STOL Service XC-142A
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