Arnold AR-5
![](http://upload.wikimedia.org/wikipedia/commons/thumb/f/f4/AR-5_Sport_Monoplane%2C_designed_and_built_by_Mike_Arnold%2C_1992_-_Hiller_Aviation_Museum_-_San_Carlos%2C_California_-_DSC03250.jpg/230px-AR-5_Sport_Monoplane%2C_designed_and_built_by_Mike_Arnold%2C_1992_-_Hiller_Aviation_Museum_-_San_Carlos%2C_California_-_DSC03250.jpg)
The Arnold AR-5 is an experimental single seat, low-wing sport monoplane with fixed conventional undercarriage, designed and built by Mike Arnold.
Development and design
[edit]Originally conceived by Mike Arnold as a personal sport airplane with excellent performance and good handling qualities. The design outperformed initial performance estimates for its relatively low power output, exceeding 200mph with only 65hp.[1] Constructed of fiberglass-epoxy matrix composite material utilizing the "moldless method" popularized by Burt Rutan.[2] Careful attention to aerodynamic detail resulted in noteworthy laminar flow drag reduction, as documented by aerodynamicists Alex Strojnik and Bruce Carmichael.[citation needed]
Legacy
[edit]In 1992, the AR-5 flown by Mike Arnold set the FAI C1a Class World Speed Record of 343,08 km/h over a 3.0km course.[3] Mike wrote several articles about his design methodology for various magazines.[4][5] The sole existing example resides at the Hiller Aviation Museum, San Carlos, CA.[6]
Specifications
[edit]General characteristics
- Wingspan: 21 ft (6.4 m)
- Wing area: 55.125 sq ft (5.1213 m2)
- Aspect ratio: 8
- Airfoil: Root: NACA 65/3-418 Tip: NACA 65/2-215
- Empty weight: 488 lb (221 kg)
- Fuel capacity: 12 Gal
- Powerplant: × Rotax 582 Inline, Liquid Cooled 2-Stroke., 65 hp (48 kW)
Performance
- Maximum speed: 213.18 mph (343.08 km/h, 185.25 kn)
- Cruise speed: 207 mph (333 km/h, 180 kn)
- Stall speed: 53 mph (85 km/h, 46 kn)
- Range: 500 mi (800 km, 430 nmi) 45 min reserve
- g limits: +6/-4g
References
[edit]- ^ "Prologue - Mike Arnold and the AR-5" (PDF). 2016-10-20. Archived (PDF) from the original on 2016-10-20. Retrieved 2021-11-22.
- ^ Factory, Rutan Aircraft (2005). Moldless Composite Sandwich Aircraft Construction. Aircraft Technical Book Company. ISBN 978-0-9774896-1-9. Archived from the original on 2022-03-04. Retrieved 2021-11-22.
- ^ "Michael S. Arnold (USA) (1097)". www.fai.org. 2017-10-10. Archived from the original on 2021-11-22. Retrieved 2021-11-22.
- ^ ""Inverse Pressure. Gradient Matching ... and other ideas for designing fast, low wing airplanes that climb and turn like mad" by MIKE ARNOLD" (PDF). Archived (PDF) from the original on 2015-09-30. Retrieved 2021-11-22.
- ^ Kitplanes (2021-07-02). "Archive: October 1999". KITPLANES. Archived from the original on 2021-11-22. Retrieved 2021-11-22.
- ^ "Hiller Aviation Museum - Models on Display". Hiller Aviation Museum. Archived from the original on 2021-11-22. Retrieved 2021-11-22.