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NASA NTRS · Other - NASA Tech Brief
Bridle Attachment for Aircraft Spin-Recovery Parachute
Attribution
This is the abstract and citation. Full text lives at NASA NTRS — we link out rather than host. All credit to the authors and Legacy CDMS.
Abstract
Verbatim from NASA NTRS. Not paraphrased, not summarized.
Antispin rolling moment produced by chute drag force. Parachute stowed prior to deployment. At deployment, bridle attachment produces antispin rolling moment. At recovery, parachute forces are in aircraft plane of symmetry. Attachment system reduces parachute diameter typically required for spin recovery of experimental aircraft during harzardous flight testing.
Author
- White, W. L.
Citation: White, W. L. (2019). Bridle Attachment for Aircraft Spin-Recovery Parachute. Legacy CDMS. NASA NTRS ID 19840000357. https://ntrs.nasa.gov/citations/19840000357 ↗