- Specifications
- See also
- References
{{DISPLAYTITLE:MacCready Gossamer Penguin}}name = Gossamer Penguin | image = Gossamer penguin.jpg | caption = Test flight of the Gossamer Penguin }}{{Infobox Aircraft Type | type = experimental aircraft | national origin = United States | manufacturer = AeroVironment | designer = Paul MacCready | first flight = 1979 | introduction = | retired = | status = | primary user = | more users = | produced = | number built = 1 | program cost = | unit cost = | developed from = Gossamer Albatross | variants with their own articles = | developed into = Solar Challenger }} |
The Gossamer Penguin was a solar-powered experimental aircraft created by Paul MacCready's AeroVironment. The Penguin was a 3/4 scale version of the Gossamer Albatross II, and had a 71 ft.(21.64 meter) wingspan and a weight, without pilot, of {{convert |68|lb |abbr=on}}. The powerplant was an AstroFlight Astro-40 electric motor, driven by a 541 watt solar panel consisting of 3920 solar cells.[2] Initial test flights were performed using a 28 cell NiCad battery pack instead of a panel. The test pilot for these flights was MacCready's 13-year-old son Marshall, who weighed {{convert |80|lb |abbr=on}}. The official pilot for the project was Janice Brown, a charter pilot with commercial, instrument, and glider ratings who weighed slightly less than {{convert | 100|lb |abbr=on}}. She flew the Penguin approximately 40 times before a {{convert | 1.95| mi |abbr=on}} public demonstration at NASA's Dryden Flight Research Center on August 7, 1980.[3] Specifications{{Aircraft specs |ref=MacCready, Lissaman, Morgan, and Burke 1983 |prime units?=kts |crew=1 |capacity= |length m= |length ft= |length in= |length note= |span m=21.64 |span ft= |span in= |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |height m= |height ft= |height in= |height note= |wing area sqm=27.6 |wing area sqft= |wing area note= |aspect ratio= |airfoil= |empty weight kg=30.8 |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity=28 x D type Nickel Cadmium (NiCad) cells or 3920 solar cells |more general= |eng1 number=1 |eng1 name=Astro-Flight Astro-40 |eng1 type=double brush DC electric motor with 133:1 reduction |eng1 kw= |eng1 hp= |eng1 note= |power original= |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note= |perfhide=Y |max speed kmh= |max speed mph= |max speed kts= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance= |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass= |more performance= }}See also{{commonscat|Gossamer Penguin}}{{Portal|Aviation|Renewable energy}}{{aircontent |related=- MacCready Gossamer Albatross
- MacCready Solar Challenger
|similar aircraft= |lists= |see also= }}References1. ^1 {{citation | publisher = NASA | place = USA | url = http://www.dfrc.nasa.gov/Gallery/Photo/Albatross/HTML/ECN-13413.html | title = Solar-powered Gossamer Penguin in flight}}. 2. ^1 {{cite book|last1=Boucher|first1=Robert, J.|title=History of Solar Flight (AIAA-84-1429)|date=June 11–13, 1984|publisher=American Institute of Aeronautics and Astronautics|location=20th Joint Propulsion Conference, Cincinnati, Ohio|url=http://arc.aiaa.org/doi/abs/10.2514/6.1984-1429|accessdate=2 February 2015}}
}}{{AeroVironment aircraft}}{{Photovoltaics}} 7 : AeroVironment aircraft|Canard aircraft|Single-engined pusher aircraft|Solar-powered aircraft|United States experimental aircraft 1980–1989|Photovoltaics|Aircraft first flown in 1979 |