Top Tweets for #HTFE25
#DefenceEGGSpurt crap
It's GTRE that R&Ds kaveri, not HAL.
#NindaTurtle MOD ##BuffoonRatna s cut funding to #GTREKaveri
With it's own funds HAL is doing #CATSWarrior, #HTT40 #IJT32Yashas #LCHPrachand & #HTSE1200 #HTFE25 engines.
#56InchFake robs HAL every year via dividends

@shiv_cybersurg Endless no IP, no R&D benefit work on total junks imported by IAF over decades like mig21, 23, 27, jaguar ,
Has destroyed independent design capabilities,
It's only HAL 's own products like #HTT40 #HTSE1200 #HTFE25 #ALHDhruv , #LCHPrachand r worth it
https://t.co/WalwH3FQaZ
HAL has screwdrivered Adour for decades - and still can't make the entire thing. Shameful. New awareness of pvt screwdrivergiri forgets how old it is
Make in India, go global: Rolls-Royce, HAL team up to build Adour engine parts
https://t.co/8bby3lIjzU

It's alive 👍
#HTFE25

Can MOD also focus on the HTFE-25 engine program that is still running on HALs Internal Funds ? . First run of this engine happened 10 years back and completion is expected only in 2030.

First run of improved PTAE-7 engines in twin engine configuration for CATS-W application completed on November 21, 2024.

HAL 25kN thrust class turbofan engine can be used on Basic / Advanced military trainers, small business jets & large UAV applications.
HTFE-25 can be used for:
- 5 ton a/c with single engine
- 9 ton a/c with twin engines
Two core engines & one full engine have been built & tested.
Core engine tested for light up, acceleration & speeds up to 99.5%.
Further trials are under progress.

HTFE-25
HTFE 25 is a low by-pass twin spool mixed flow turbofan engine, being developed by AERDC, HAL. It has a 3 stage LP compressor, 5 stage HP compressor and air cooled high efficient turbine blades. It is a medium thrust class engine

@MysticOwl7 Hello, the unroll you asked for: @nileshjrane: 1. @HALHQBLR embarked upon development of two engines about 5yrs ago. #HTFE25 and #HTSE1200. HAL's… https://t.co/IeuMPZ2BZP Enjoy :) 🤖
@MysticOwl7 Hi! please find the unroll here: @nileshjrane: 19. UPDATE HAL AR 2018-19: #HTFE25 core has two prototype under test - Core-1 and Core-2. FY2018-19 saw… https://t.co/KStS5cuJWc Enjoy :) 🤖
17. #HTFE25 started in 2013-14 with 6yr timeframe. Current status - Core 2 runs completed. Now Full Engine TD runs and Design Config review in progress.
No order yet, but product specific dev (e.g. for IJT or Jaguar) would take another 5yr, which is what I had expected too.

@Power_monger Hi! there is your unroll: Thread by @nileshjrane: "19. UPDATE HAL AR 2018-19: core has two prototype under test - Core-1 and Core-2. FY2018-19 saw 96 test runs bri […]" #HTFE25 #HTFE https://t.co/KStS5cuJWc
Have a good day. 🤖
9. #HTFE25
Thrust = 25kN Dry, close to 40kN wet
SFC = 0.71 kg/kgf.hr
T/W ratio = 5.66
MFR = 43 kg/s
BPR = 0.5
OPR = 20.43
Max TET = 1450 K
Max Op alti = 11km
Relight envelop = 0-9 km
Weight ~ 450kg
Config = 3 LPC - 5 HPC - 1 HPT - 1 LPT

9. #HTFE25 feature -
- Modular construction
- wide chord fan blades
- High efficiency Compressor with VIGVs
- Advanced annular combustor
- Air cooled high efficiency turbines (3D printed HPT nozzle & rotor blades)
- Dual channel FADEC with Health Usage and Monitoring System HUMS
8. #HTFE25 has 25kN thrust in dry mode which can be enhanced to 36-40kN once an afterburner is fitted in it. This makes it an ideal engine for ~5T class single engine aircrafts such as Trainers like IJT Sitara or ~9T class combat fighters such as Jaguar or some for a Business Jet
6. #HTFE25 went on testbed for its first test run sometime in 2015. Fast forward to 2018, it had two prototypes which had completed 255 test runs as per HAL's last Annual Report. #AeroIndia2019 brings some updates on the engine. In the first step the core of the engine has been
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