1967-02-01

OV-10A Landing Gears 670562

OV-10A LANDING GEARS - The landing gears of the OV-10A have been designed to meet extremely severe landing and operating conditions. The articulated main gear and semi-articulated nose gear assemblies have proven to be well suited to meeting the requirements for high sink rate landings onto bumps, steps and holes in addition to taxiing and making take-offs over undulating contours. Development data on the landing gear shock struts in laboratory airframe drops and actual flight test landings show good agreement with predicted performance.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.

Due to current capacity constraints, printed versions of our publications - including standards, technical papers, EDGE Reports, scholarly journal articles, books, and paint chips - may experience shipping delays of up to four to six weeks. We apologize for any inconvenience.
We also recommend:
TECHNICAL PAPER

F-106B Airplane Active Control Landing Gear Drop Test Performance

901911

View Details

TECHNICAL PAPER

Simulation of Aircraft Landing Gear Dynamics Using CATIA, CATDADS, DADS and NASTRAN at Cessna Aircraft

2000-01-1699

View Details

TECHNICAL PAPER

F-15 Nose Landing Gear Shimmy, Taxi Test and Correlative Analyses

801239

View Details

X