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Active Blowing Force Measurement System Development
Active Blowing Force Measurement System Development

NTF Semi-Span Active Flow Control Calibration System at NASA’s Langley Research Center National Transonic Facility.

Balance Flexure Fillet Study Research
Balance Flexure Fillet Study Research

Balance Flexure Fillet Study research specimen being tested at NASA’s Langley Research Center.

Semi-Span Balance Development and Calibration Capabilities
Semi-Span Balance Development and Calibration Capabilities

New 30,000 lb normal force (lift) semi-span balance designed by NFMTC for NASA Ames Research Center’s 11-foot transonic wind tunnel…

Semi-Span Balance Development and Calibration Capabilities
Semi-Span Balance Development and Calibration Capabilities

Large Load Rig (LLR) Semi-span Calibration System at Triumph Force Measurement Systems in San Diego, Calif.

Single Vector System (SVS)
Single Vector System (SVS)

Single Vector System (SVS) used to calibrate small- to medium-capacity internal balances at NASA’s Langley Research Center.

Internal Balance for the Hybrid Wing Body Model
Internal Balance for the Hybrid Wing Body Model

New 5.0-inch-diameter internal balance for the hybrid wing body model tested at NASA’s Langley Research Center’s 14- by 22-Foot facility.

Balance Check Calibration Cart
Balance Check Calibration Cart

Balance Check Calibration Cart at NASA’s Glenn Research Center.

Balance Check Calibration Cart
Balance Check Calibration Cart

Balance Check Calibration Cart at NASA’s Langley Research Center.

Methane-Powered 3-D Printed Turbopump: Heart of an Engine
Methane-Powered 3-D Printed Turbopump: Heart of an Engine

Working much like a human heart, a rocket’s turbopump is a complex engine component that pumps fuel into an engine.…