Transcription of DTIC
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N l USAAVSCOM TR 89-o-11 FILE COPYNVUS ARMYI AVIATIONSYSTEMS COMMANDADVANCED TECHNOLOGY landing GEARV olume I SenMcDonnell Douglas Helicopter Company DTIC5000 East McDowell RoadMesa, AZ 85205 ELECTEA ugust 1990 Report for Period September 1985 -December 1989 Approved for public release; distribution Is forAVIATION APPLIED TECHNOLOGY DIRECTORATEUS ARMY AVIATION SYSTEMS COMMANDFORT EUSTIS, VA 23604-5577 AVIATION APPLIED TECHNOLOGY DIRECTORATE POSITION STATEMENTThe objective of the Advanced Technology landing gear (ATLG) Programwas to design, fabricate, and test a crashworthy retractable main landinggear system suitable for an 8500-pound utility helicopter.
The landing gear is of a tricycle configuration and is designed to absorb 60 percent of the energy from a 42 fps level impact condition. The landing gear extends automatically
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11: Landing Gear & Components, Landing gear, CHAPTER 32 - Landing Gear, CHAPTER 32 LANDING GEAR, Components, Chassis Parts Manual, LANDING GEAR COMPONENTS, Landing Gear Landing Gear Landing Gear, CRJ 700/900 Landing Gear, DELTA, Chapter 8 Weight Estimation, CHAPTER 13 LANDING GEAR, Landing Systems, Chapter 3 Landing Gear Concept Selection