Engineering:HAL HTSE-1200

From HandWiki
Revision as of 17:59, 17 December 2022 by MainAI5 (talk | contribs) (fix)
(diff) ← Older revision | Latest revision (diff) | Newer revision → (diff)
HTSE-1200
HTSE 1200 turboshaft engine model.png
HTSE 1200 Turbo-shaft engine model
Type Turboshaft
National origin India
Manufacturer Hindustan Aeronautics Limited
First run 12 February 2018[1]
Major applications HAL Dhruv
HAL Rudra
HAL Light Combat Helicopter
HAL Light Utility Helicopter

The HAL HTSE-1200 ("Hindustan Turbo Shaft Engine") is a turboshaft engine under development by India's Hindustan Aeronautics Limited (HAL). It is aimed at 3.5 ton single engine class and 5-8 ton twin engine class helicopter configurations. India will need 5,000-6,000 helicopters to operate in 2020s.[2] This will be an indigenous design giving engine alternatives for the HAL-developed LUH, ALH and LCH.[3] The first run of engine was conducted in February 2018 when it achieved 76% of the rpm required.

There have been 250 tests of engine since inaugural run. The engine has been "progressing well" to have its first flight test by end of 2019. Directionally Solidified Gas Generator (GG) Turbine blades were also developed for the engine indigenously.[1][4][5]

Specifications (HTSE-1200)

Data from [6]

General characteristics

  • Type: turboshaft
  • Length: 51.18 inches (1.300 m)
  • Diameter:
  • Dry weight: 235 kilograms (518 lb)

Components

Performance

See also

Related development

Comparable engines

  • LHTEC CTS800
  • MTR390
  • Pratt & Whitney Canada PT6
  • Safran Arrano

Related lists

References