About: NASA Puffin

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An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The Puffin is an American proposed hover-capable, electric-powered, low-noise, personal vertical takeoff and landing (VTOL) technology-concept proprotor aircraft. The concept design was projected to be capable of flying a single person at a speed of 150 miles per hour (241 km/h), with range expected to be less than 50 miles (80 km) with 2010-vintage Lithium-iron-phosphate battery technology. The design specified a 13.5 foot (4.1 m) wingspan, standing 12 feet (3.65 m) tall on the ground in its take-off or landing configuration.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	NASA Puffin
rdfs:comment	The Puffin is an American proposed hover-capable, electric-powered, low-noise, personal vertical takeoff and landing (VTOL) technology-concept proprotor aircraft. The concept design was projected to be capable of flying a single person at a speed of 150 miles per hour (241 km/h), with range expected to be less than 50 miles (80 km) with 2010-vintage Lithium-iron-phosphate battery technology. The design specified a 13.5 foot (4.1 m) wingspan, standing 12 feet (3.65 m) tall on the ground in its take-off or landing configuration.
sameAs	dbr:NASA_Puffin
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range km	80(xsd:integer)
Status	One-third scale model built, not flown
range miles	50(xsd:integer)
Type	Personal electric aircraft
span m	4(xsd:double)
See Also	*Electric aircraft
max speed kmh	241(xsd:integer)
length m	3(xsd:double)
max speed mph	150(xsd:integer)
National Origin	United States
length ft	12(xsd:integer)
span ft	13(xsd:double)
range note	expected range "no more" than this
prime units?	imp
Crew	1(xsd:integer)
Number Built	0(xsd:integer)
ref	NASA
abstract	The Puffin is an American proposed hover-capable, electric-powered, low-noise, personal vertical takeoff and landing (VTOL) technology-concept proprotor aircraft. The concept design was projected to be capable of flying a single person at a speed of 150 miles per hour (241 km/h), with range expected to be less than 50 miles (80 km) with 2010-vintage Lithium-iron-phosphate battery technology. The design specified a 13.5 foot (4.1 m) wingspan, standing 12 feet (3.65 m) tall on the ground in its take-off or landing configuration.

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