*Âü°í ½ÎÀÌÆ®-http://www.flug-revue.rotor.com/FRTypen/FRHJT-36.htm
2005³â ¾Æ¿¡·Î Àεð¾Æ 2005¿¡ °ø°³µÈ ½ÅÇü Áßµî ÈƷñâ·Î ±âÁ¸ÀÇ HAL HJT-16 Mk.IA and Mk.II ÈƷñ⸦ Á¡Â÷ÀûÀ¸·Î ´ëüÇÒ °ÍÀ̸ç, °íµî ÈƷñâ ȣũ±â¿Í ÀÚ±¹»ê LCA ÀüÅõ±âÀÇ Áß°£ ¼º´ÉÀÌ µÉ °ÍÀ̶ó°í ¿¹»óÇÏ°í ÀÖ½À´Ï´Ù.
LCA 40´ë »ý»ê¿¡ ´ëÇÑ ¾çÇØ°¢¼(MOU)¸¦ ü°áÇϱ⵵ ÇÑ Àεµ´Â Áß±¹°ú ´õºÒ¾î ¾Æ½Ã¾ÆÀÇ ÇÙÀ¸·Î °·ÂÈ÷ ºÎ»óÇÏ°í ÀÖ½À´Ï´Ù.
Á¶±Ý ¼º±ÞÇϱâ±îÁöµµ ÇÑ MCA±îÁö ³ª°¡°í ÀÖÁ®...
¹é¸¶µð ¸»º¸´Ù ÇѹøÀÇ ÇൿÀÌ Àý½ÇÇÑ ½ÃÁ¡¿¡ Àεµ´Â ¼ºÅ ¼ºÅ ÇൿÀ¸·Î ¿Å±â°í ÀÖ½À´Ï´Ù...
Á¶·Õº¸´Ù´Â ºÎ·¯¿öÇؾßÁ®..
Àú ±¹Åä¿¡ Àú Àα¸°¡ Çѹø ¿òÁ÷ÀÎ´Ù´Â°Ô ´ë´ÜÇÏÁö¿© Æı«·ÂÀº µÎ¸»Çϸé ÀܼҸ®°í...
General (Allgemeine Angaben)
Crew (Besatzung): 2, on Zvezda K36LT ejection seats
Weapons: No details known but there are four underwing hardpoints and one hardpoint under the fuselage
Power plant (Antrieb): 1 x Snecma Larzac 04H20 turbofan (no afterburner)
Thrust (Schub): 14,03 kN (3153 lbs)
--------------------------------------------------------------------------------
Dimensions (Abmessungen)
Length (Länge): 10,91 m
Height (Höhe): 4,13 m
Span (Spannweite): 9,80 m
Wing sweepback (Flügelpfeilung): 18 deg on the leading edge
--------------------------------------------------------------------------------
Weights (Massen)
Max. external load (max. Au©¬enlasten): 1000 kg
Take-off weigth (Startmasse):
- clean (ohne Au©¬enlasten) 3500 kg
- maximum: 4500 kg
--------------------------------------------------------------------------------
Performance (Flugleistungen)
Max. level speed (max. Fluggeschwindigkeit): Mach 0.8
Max. dive speed (max. Geschw. im Sturzflug): 825 km/h
Service ceiling (Dienstgipfelhöhe): 12000 m (39360 ft)
Endurance (Flugdauer): 3 h
g limits: +8/-3 g
The HAL HJT-36 'Sitara' Intermediate Jet Trainer (IJT) is the slated replacement for the HAL HJT-16 Mk.IA and Mk.II trainers in IAF service. Only two prototypes (S-3466 and S-3474) exist and HAL brought both of them to the show, .perhaps to make up for the broken promise of flying the first HJT-36 prototype at Aero India 2003. Additional prototypes aren't likely to be built as HAL maintain that only two are required to complete the entire development phase of programme. Motivated by the speed and success of the latter and an estimation that the IAF would need more than the 66 Hawk AJTs on order, HAL also announced their initiative to develop the HJT-39 Combat Attack Trainer (CAT), for the AJT and secondary ground attack roles. A full scale forward fuselage and glass cockpit mockup of the CAT was displayed, the former almost exactly matching the HJT-36's forward fuselage and nose shape. The aircraft is expected to fly 44 months after the go-ahead. The mockup of this aircraft type was first displayed at Aero India 1998 and two prototypes are now flying at the same show, a few years later. Will the same happen with the HJT-39?
1. S-3466 is the first prototype of the HJT-36 and initially flew with only one seat, the instructor's seat being replaced with flight test instrumentation. This aircraft mainly remained on static display and occasionally flew on demonstration sorties, not a part of the actual air display, which was left to the second prototype.
2. S-3466 also had no HUD in the beginning but now adorns a HUD from Thales. The cockpit of dial pointer instruments is also to be standardized to the level of the one on the second prototype. This machine completed 81 sorties/55 hrs of flight by mid-January 2005.
3. The second, brighter looking, prototype (S-3474) arrives at the show. The aircraft encountered a minor glitch when it's tyre burst on the tarmac, one day before the show but this was immediately remedied in time for it's flyby at the inauguration and other days.
4. S-3474 had only completed 46 sorties/27 hrs of flying by mid-Jan 2005 but put together an awesome display of maneuvers and aerobatics. This was also despite being underpowered with the Larzac, compared to their production standard thrust requirements. If the solo demonstration was so impressive, one wonders what the Surya Kirans would achieve with this aircraft?
5. The mockup of the HJT-39 CAT's cockpit shows the indigenous CSIO/BEL-developed HUD and UFCP, used on the LCA. At this stage, the CAT appears to be little more than a twin-engined HJT-36 in terms of shape. Before their actual formal proposal, HAL had announced the potential of an improved HJT-36 derivative.
´ñ±Û [1]
½ÃÁöÇÁ½º | 2005-05-14 | Ãßõ 0