Row 2732

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{
  "text": "HMAS is a comprehensive program to develop an advanced fighter aircraft and individual critical components. We will try to include a complex of developments in one post\n\nEngines HE-414, HE-416\nHAL is spinning off its engine manufacturing division into a separate subsidiary, HE (Hindustan engines). Structural separation is necessary to concentrate the separate staff and finances of an individual company on its narrow task. HE is currently producing AFL-31 engines for the Su-30MKI and is preparing to open production of the GE-414 according to a previously reached agreement (https://idrw.org/f-414-hal-to-get-80-tot-ge -lists-out-tot-details/). The Indian version of the engine will receive the HE-414 index and the following characteristics\n\nThrust normal 57.8 kN\n\nThrust max 98 kN\n\nDry weight 1,110 kg\n\nLength 391 cm\n\nMaximum diameter 89 cm\n\nInlet diameter 79 cm\n\nThrust-to-weight class 9:1\n\nThis engine will form the basis for the upcoming Tejas Mk2 and HMAS prototypes. Production launch is planned for 2028\n\nNext, HE is tasked with developing a more powerful version of this engine. The new engine should retain the dimensions of the old one, but increase power by 25%. The engine will receive the index HE-416 and the following characteristics\n\nThrust normal 91 kN\n\nThrust max 137 kN\n\nDry weight 1,350 kg\n\nLength 391 cm\n\nMaximum diameter 89 cm\n\nInlet diameter 79 cm\n\nThrust-to-weight class 9.2:1\n\nIt is expected that the engine will form the basis for production HMAS aircraft and will also be used to re-engine the Tejas Mk2 in future updates. We will also accept GE's help in developing a new engine if they agree to help. The estimated completion date for development is 2032-2033. Completion of testing and certification – 2035-2036\n\n\nUttam Mk3/Mk10/Mk15\n\nThe Uttam radar family will continue to develop. The Uttam Mk2, which is being prepared for installation on the new Tejas Mk2, is a powerful Indian-made radar that uses many modern technologies including AESA and ultra-thin side section. However, the radar cannot be called the best, largely due to its limited size. The canvas has only 968 TRM, which is normal for a light fighter, but there is no talk of superiority. Moreover, the radar modules are made of GaAs, which is also not the best technology available. The Uttam family will continue to develop.\n\nUttam Mk3\nAntenna substrate diameter – 900 mm\nNumber of TRMs – 1850\nTRM material – GaAs\nAvailability of AESA, electronic warfare, high-speed communications, high-resolution terrain mapping mode, identification and tracking of ground targets, ultra-thin antenna side section.\nThis radar is a continuation of the scaling of already proven Uttam radar technologies, and therefore does not require fundamentally new research. This radar is intended for use on HMAS prototypes, on production HMAS if the Mk15 is not ready on time, as well as for the potential modernization of the Su-30MKI, if such a decision is made. This radar is sized to fit the nose cone of the Su-30MKI. The estimated date of completion of work and readiness for mass production is 2030.\n\nUttam Mk10\n\nAntenna substrate diameter – 650 mm\nNumber of TRMs – 1648\nTRM material – GaN\nAvailability of all functions of previous models of the family\nUttam Mk10 is a fundamentally new radar in the family. The use of GaN significantly expands the temperature range of the radar, allowing for additional TRM densification and increased overall system performance. This radar also uses the most advanced available technologies for compacting antenna modules, which was previously used in India only on experimental samples. Radar will require significant hardware development effort, but the software part should not lag behind. Data processing will be distinguished by a new on-board computer with increased performance, which will allow you to extract the maximum useful data from the received signals. BEL (developer of Uttam radar) will have to do a lot of work for this. The Uttam Mk10 matches the dimensions of the Uttam Mk2 radar that will be installed in the Tejas Mk2 and will potentially replace it in future updates. The estimated completion date for development is 2035. Completion of testing and readiness for serial production - 2037-2038\n\nUttam Mk15\n\nAntenna substrate diameter – 900 mm\n\nNumber of TRMs – 2344\n\nTRM material – GaN\n\nPresence of all functions of the previous radar + electro-hydraulic system for mechanical antenna rotation\nUttam Mk15 is a scaled version of Uttam Mk10, combined with a mechanical antenna rotation system. The radar uses the same technology base, but is larger in size. The development of both radars will proceed in parallel. Uttam Mk15 is intended for use in production HMAS aircraft. The advanced capabilities of the rotary radar will allow the fighter to play the role of mini-AWACS, controlling manned or unmanned wingmen on a battlefield remote from it, which will be one of the main tasks of the promising vehicle. The estimated completion date for development is 2036. Completion of testing and readiness for serial production - 2037-2038\n\n\nPOD BEL Baaz\nBEL is tasked with developing a state-of-the-art detection and targeting module, BEL Baaz. The military command requires a viewing range of 80+ km, black-and-white, color and thermal imaging, advanced capabilities for determining distance, position in the GPS system, laser guidance for static and dynamic targets. This requires the use of advanced optronics, modern data processing algorithms and post-processing using AI. It is possible to create an initially intermediate version with more modest characteristics for testing technologies. We welcome cooperation in development with our long-time Israeli partners and the possible involvement of new partners. The Baaz will be suspended from a standard fighter pylon and will significantly increase its lethality against ground targets. These same technologies will form the basis of the optics of our promising UAVs\n\n\nHMAS\nHMAS is the general name for the program to develop a promising fighter aircraft and advanced modules for Indian aviation. We’ve already talked about the main modules, now it’s time for what everything was started for. Military designation will be assigned later\n\nHMAS\n\nCrew 2 people\n\nLength – 19.5 m\n\nWingspan - 14.5 m\n\nWing area – 83.3 m\n\nEmpty weight – 18,000 kg\n\nFuel weight – 12,000 kg\n\nPayload - 10,000 kg\n\nMaximum take-off weight – 40,000 kg\n\nAirframe materials:\n\nTitanium alloys – 45%\n\nComposites – 30%\n\nEngines – HE-416x2 (137 kNx2) (on production vehicles)\n\nThrust-to-weight ratio in air-to-air operations – 1.01\n\nThrust-to-weight ratio with maximum take-off weight – 0.62\n\nMaximum speed – 2.3 M at altitude\n\nFlight ceiling – 20,000 m\n\nCombat radius without EFT – 1,500 km\n\n\nHMAS-N (Naval)\n\nCrew 2 people\n\nLength – 19.5 m\n\nWingspan - 14.8 m\n\nWing area – 85.8 m\n\nEmpty weight – 20,000 kg\n\nFuel weight – 12,000 kg\n\nPayload - 8,000 kg\n\nMaximum take-off weight – 40,000 kg\n\nAirframe materials:\n\nTitanium alloys – 45%\n\nComposites – 30%\n\nEngines – HE-416x2 (137 kNx2) (on production vehicles)\n\nThrust-to-weight ratio in air-to-air operations – 0.92\n\nThrust-to-weight ratio with maximum take-off weight – 0.62\n\nMaximum speed – 2.3 M at altitude\n\nFlight ceiling – 20,000 m\n\nCombat radius without PTB – 1,500 km\n\n\nHMAS will be built according to a normal aerodynamic design with a diamond-shaped wing with a developed leading edge of the wing. The airframe will have widely spaced engines, between which there are 2 internal weapon compartments. The compartments have a length of 8.3 m and a width and depth of 0.65 m. Together, this makes it possible to place up to 8 air-to-air missiles of the Astra family or up to 2 heavy suspensions similar to air-launched cruise missiles. Two more points for heavy suspensions are located under the engine nacelles. There are 2 more suspension points under the wings - 1 close to the fuselage and 2 in the center of the wing with double and triple pylons, respectively. Instead of a double one, there is one heavy suspension. In total, the aircraft has a maximum of 20 suspension points, 2 of which are for heavy suspensions, or 12 points, 6 of which are heavy. The aircraft must have characteristic stealth shapes to deflect reflected radio waves, as well as a coating of radio-absorbing composites. The coating should be oriented towards wear resistance, even at the expense of radio absorption. No additional applied coating required\n\n\nThe avionics are primarily represented by the Uttam Mk15 radar, a new on-board computer, an advanced human-machine interface, large-scale automation of flight control and information collection while maintaining the pilot’s key role in decision making, and control of the main aircraft systems using the pilot’s helmet. The integrated modular electronic warfare system can enhance its capabilities using the potential of the Uttam Mk15. The key requirement for the system is seamless interaction of electronic warfare modules of various aircraft to scale electronic warfare capabilities. The fighter must implement individual thrust control for each engine to increase the aircraft's maneuverability\n\nExpected development completion date – 2033\n\nExpected completion date of testing – 2037\n\nUnit cost - $120 million",
  "label": "r/globalpowers",
  "dataType": "post",
  "communityName": "r/GlobalPowers",
  "datetime": "2023-11-28",
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}

Entry Information

• Entry ID: 2732
• Repository: Axioma AXP
• Dataset: arrmlet/reddit_dataset_36
• Total Entries: 100,000