1995-09-01

Orbiter Tire Traction and Wear 952019

The traction and wear problem for a main landing gear tire of the Space Shuttle Orbiter is considered. Side force acting on the tire during landing under yawed conditions, and the associated tire wear, are computed using analytical expressions derived from basic principles of physics. These equations relate side traction and wear to vertical contact load, slip angle, tire mechanical properties, footprint geometry, and rubber abradability. Numerical results in graphical form are presented for side force as a function of slip angle at various tire loads and compared with values obtained using the empirical formula of Dryden Flight Research Center (DFRC). Energy dissipated by the side force is used as a tire-wear index, forming the basis for deriving bilinear tire wear models for both the Kennedy Space Center (KSC) and Edwards AFB runways. The constants of these models are determined using Convair 990 (CV 990) Landing Systems Research Aircraft (LSRA) test data.

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.
We also recommend:
STANDARD

Aircraft Tire Inspection - In-Service Removal Criteria

ARP6225A

View Details

STANDARD

Steering Effect of Tilted, Free-Swiveling Nose Gears

AIR4358

View Details

STANDARD

Recommended Practice for Measurement of Static and Dynamic Characteristic Properties of Aircraft Tires

ARP4955A

View Details

X