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Boom Supersonic XB-1 nears supersonic flight after passing stability test

Aerotime

The test focused on testing the aircraft’s handling qualities without the stability augmentation system (SAS) activated. Boom Supersonic Boom Supersonic Boom Supersonic Boom Supersonic The post Boom Supersonic XB-1 nears supersonic flight after passing stability test appeared first on AeroTime.

Stability 268
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Boom Supersonic’s XB-1 demonstrator completes second test flight

Aerotime

This included testing the retraction and extension of the landing gear, as well as assessing a digital stability augmentation system known as a roll damper to enhance in-flight stability. Additionally, tufting, a technique used to visualize airflow, was applied to the right wing to ensure aerodynamic performance.

Stability 261
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Boom Supersonic XB-1 Completes Successful Second Test Flight

AV Web

During its second test flight, XB-1 flew for about 15 minutes, reaching an altitude of 10,400 feet and speeds of 232 knots. The test also focused on assessing the aircraft’s handling qualities and activating a new digital stability augmentation system, or roll damper.

Stability 109
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Italian Fare

Plane and Pilot

/hp Engine: Rotax 912iSC3, 4-cylinder, opposed, air and liquid cooled, normally aspirated, gear-reduction drive, fuel-injected, 100 hp Propeller: MT composite, two-blade, constant-speed Maximum Cruise Speed: 117 knots Range, Max Range Power: 950 nm Rate of Climb, Sea Level: 750 fpm Max operating Altitude: 13,000 ft. Takeoff Over 50-ft.

Knot 71
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Airspeed and Altitude Control Simplified: Tips for Stable Flying

Pilot Institute

It’s typically measured in knots (nautical miles per hour), with one knot being about 1.15 As an aircraft accelerates, especially at or above 200 knots, the air particles flowing around it become tightly packed. Although they each provide specific information, using them together will give you a better picture of your stability.

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Bargain Buys on AircraftForSale: 1975 Cessna 150M

Plane and Pilot

Among the various 150 subtypes produced over the years, this late-model example is visually defined by its modern-looking swept vertical stabilizer and large rear windows. This compares to earlier models that had large, straight vertical stabilizers and a “fastback” design that provided no rearward visibility.

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Split-S Decision

Plane and Pilot

Alongside a nearby highway, some recognizable bits of airplane, the vertical stabilizer and rudder, a horizontal stabilizer and elevator, fell separately to Earth. But a review of the avionics data shows it was entered at the correct airspeed (placarded as between 104 and 165 knots), and the roll rate was constant.