About: HAL HT-2

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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 Hindustan HT-2 is an Indian two-seat primary trainer designed and built by Hindustan Aeronautics Limited. The HT-2 was the first company design to enter production in 1953 for the Indian Air Force and Navy. The HT-2 is a low-wing cantilever monoplane with a fixed tailwheel landing gear. Powered by a 155 hp (116 kW) Cirrus Major III piston engine the aircraft has enclosed tandem cockpits with dual controls. Apart from military use the aircraft was also used by Indian flying schools.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	HAL HT-2
rdfs:comment	The Hindustan HT-2 is an Indian two-seat primary trainer designed and built by Hindustan Aeronautics Limited. The HT-2 was the first company design to enter production in 1953 for the Indian Air Force and Navy. The HT-2 is a low-wing cantilever monoplane with a fixed tailwheel landing gear. Powered by a 155 hp (116 kW) Cirrus Major III piston engine the aircraft has enclosed tandem cockpits with dual controls. Apart from military use the aircraft was also used by Indian flying schools.
sameAs	dbr:HAL_HT-2
empty weight kg	699(xsd:integer)
dcterms:subject	dbkwik:resource/0Yft4JxlC0uEtP96vrJKew== dbkwik:resource/hBYxR6Ih4x0dwFOQqlJ_JA==
dbkwik:military/pr...iPageUsesTemplate	dbkwik:resource/AaGpNMKXeCEx6k1ovZIRVg== dbkwik:resource/8c65HClsHBgkxfJdWXaRHw== dbkwik:resource/gU9hsdlj38XEAqgU2NtQ_g== dbkwik:resource/7_dwHHF8FUA3XhGjI4-8Fw== dbkwik:resource/LotLVatVmnPAGa3qNFT_3g== dbkwik:resource/dLGY2ypVsQBpZ71XpuCB9g==
ceiling ft	14500(xsd:integer)
met or eng?	eng
eng1 type	Cirrus Major III piston engine
endurance h	3(xsd:integer)
gross weight kg	1016(xsd:integer)
length in	8(xsd:integer)
endurance min	30(xsd:integer)
primary user	Indian Air Force
Type	Two-seat primary trainer
eng1 kW	116(xsd:integer)
wing area sqft	172(xsd:double)
height m	2(xsd:double)
Height in	11(xsd:integer)
span m	10(xsd:double)
Manufacturer	Hindustan Aeronautics Limited
empty weight lb	1540(xsd:integer)
ceiling m	4420(xsd:integer)
cruise speed kmh	185(xsd:integer)
length m	7(xsd:double)
length ft	24(xsd:integer)
Height ft	8(xsd:integer)
First Flight	--08-05
span ft	35(xsd:integer)
cruise speed mph	115(xsd:integer)
gross weight lb	2240(xsd:integer)
span in	2(xsd:integer)
wing area sqm	16(xsd:integer)
Crew	2(xsd:integer)
eng1 hp	155(xsd:integer)
ref	The Illustrated Encyclopedia of Aircraft , 1985, Orbis Publishing, Page 2172
eng1 number	1(xsd:integer)
abstract	The Hindustan HT-2 is an Indian two-seat primary trainer designed and built by Hindustan Aeronautics Limited. The HT-2 was the first company design to enter production in 1953 for the Indian Air Force and Navy. The HT-2 is a low-wing cantilever monoplane with a fixed tailwheel landing gear. Powered by a 155 hp (116 kW) Cirrus Major III piston engine the aircraft has enclosed tandem cockpits with dual controls. Apart from military use the aircraft was also used by Indian flying schools.

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