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Pegasus Hypersonic Experiment

The Pegasus Hypersonic Experiment was a NASA flight-research investigation built around a smooth, instrumented steel glove fitted to the first-stage wing of a Pegasus booster. Its pressure, temperature, hot-film, and acceleration sensors characterized the transition from laminar to turbulent airflow during ascent at hypersonic speed.

Pegasus Hypersonic Experiment
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Identity

Aliases
PHYSXPegasus wing-glove experimentHypersonic glove experiment
Name
Pegasus Hypersonic Experiment
Status
completed

Details

Astronauts
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Description
The Pegasus Hypersonic Experiment was a NASA flight-research investigation built around a smooth, instrumented steel glove fitted to the first-stage wing of a Pegasus booster. Its pressure, temperature, hot-film, and acceleration sensors characterized the transition from laminar to turbulent airflow during ascent at hypersonic speed.
End Date
1998-10-22
Launch Site
Outcome
The wing glove collected approximately ninety seconds of aerodynamic and thermal measurements as Pegasus accelerated toward Mach 8. Because the first stage was expendable, the experiment processed and transmitted its data in real time, producing usable boundary-layer-transition results for comparison with design and stability models.
Programs
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Start Date
1998-10-22
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Creation Time
July 18, 2026 at 16:58:57 UTC
Updated Time
July 29, 2026 at 08:55:06 UTC

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Pegasus Hypersonic Experiment PHYSX Pegasus wing-glove experiment Hypersonic glove experiment
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