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GRIPEN NG (SU-35 KILLER)

SU-27 VS F-15

Insane Low Passes by Skilled Pilots




Supersonic Flight, Sonic Booms

SU35 vs F22 RAPTOR vs EUROFIGHTER 2013

The best of crazy fighter aircraft pilots

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Mecca and Medina with 360-degree panorama from your computer or mobile phone

Mecca and Medina with 360-degree panorama 

from your computer or mobile phone

(youtube : The New York Times)

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MELIHAT MEKAH & MADINAH DARI LAYAR HANDPHONE ATAU KOMPUTER DARI BERBAGAI SUDUT SECARA 360 DERAJAT

MELIHAT MEKAH & MADINAH 

DARI LAYAR HANDPHONE ATAU KOMPUTER 

DARI BERBAGAI SUDUT SECARA 360 DERAJAT

(sumber youtube : The New York Times)

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IBARAT JANUR BELUM TERPASANG - GRIPEN PANTANG MENYERAH MESKI INDONESIA TELAH MEMILIH SUKHOI

Indonesia Pilih Sukhoi, Pabrikan Pesawat Gripen Tak Menyerah  

Berikut ini kemampuan teknis dari pesawat Gripen, kecepatan terbang mencapai mach 2 dengan combat radius mencapai 800 km saja, namun jika harus terbang ferry mencapai jarak 3.200 Km. Ketinggian terbang mencapai 15 km, dengan tekanan beban gravitasi mencapai 9 G. Saabgripen.com

Keputusan Pemerintah Indonesia memilih pesawat tempur asal Rusia, Sukhoi SU-35 dua minggu lalu menjadi pukulan berat bagi pabrikan alat pertahananan asal Swedia, Svenska Aeroplan AB (SAAB). Pasalnya, sejak TNI Angkatan Udara merencanakan mengganti jet buru sergap F-5 Tiger mereka tiga tahun lalu, SAAB gencar mempromosikan pesawat andalan mereka, Gripen.

Walau pemerintah lebih memilih Sukhoi, SAAB mengaku belum kehilangan harapan untuk mengikat kontrak dengan pemerintah Indonesia. "Kami optimistis dan tak akan menyerah. Kami adalah tawaran terbaik bagi Indonesia," ujar Direktur Kampanye Gripen dan Airborne System SAAB Asia-Pasific Magnus Hagman, saat ditemui Tempo di Singapore Airshow 2016, Kamis, 18 Februari 2016.

Magnus mengibaratkan pembelian pesawat seperti sebuah gunung es, 20 persen bagian di permukaan adalah harga pembelian. Yang masih sering luput dalam perhitungan adalah biaya perawatan, pengaturan, operasional, inventory,technical support, pelatihan, serta disposal. "Penelitian IHS Jane's Defense Weekly tentang itu semua menunjukan biaya Gripen paling murah, yaitu US$ 4,7 ribu per jam," kata dia.

Ditemui pada saat yang bersamaan, Kepala Kantor Perwakilan SAAB Indonesia Peter Calrqvist mengatakan anggaran sebesar itu tidak akan menggerogoti anggaran pertahanan dibanding dengan pesawat lainnya. "Pesawat lain yang biaya operasionalnya tinggi akan memakan anggaran pertahanan dan berefek jarang terbang," kata Peter.

Mereka berencana mengunjungi kembali Indonesia untuk bertemu dengan TNI. Sebuah paket khusus sudah mereka siapkan untuk ditawarkan bagi TNI.

Sebelumnya, Menteri Pertahanan Ryamizard Ryacudu berencana melakukan kunjungan kerja ke Moscow, Rusia, Maret mendatang. Menurut dia, pemerintah akan membeli delapan hingga sepuluh unit pesawat Sukhoi SU-35.

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SU-35 PESEN SEKARANG - DATANGNYA 5 TAHUN KEMUDIAN

PERKEMBANGAN TEKNOLOGI MEMANG BEGITU SANGAT CEPAT. SEPERTI MENTERI PERTAHANAN BILANG JIKA KITA MEMESAN SU-35 SEKARANG MAKA AKAN BARU DATANG 5 TAHUN KEMUDIAN. SEDANGKAN PADA 5 THN YANG AKAN DATANG TEKNOLOGI PESAWAT TEMPUR JUGA SUDAH MENGALAMI PERUBAHAN DAN PERBAIKAN PADA VERSI-VERSI SEBELUMNYA

BUTUH PENGKAJIAN MENDALAM DARI BERBAGAI ASPEK DAN SISI LAINNYA UNTUK MENJAGA KEDAULATAN WILAYAH NKRI YANG LUAS INI.

PERLU KUALITAS DAN KUANTITAS. 

SYSTEM TRANSFER TEKNOLOGI UNTUK MEMBERDAYAKAN SUMBER DAYA ANAK BANGSA AGAR BISA MANDIRI DAN IKUT BERKANCAH DI AKUI OLEH DUNIA

PERLU PENINGKATAN ANGGARAN. SETIDAKNYA ANGGARAN YANG STABIL AGAR PERENCANAAN DAN EFISIENSI PELAKSANAAN OPERASIONAL TETAP TERJAMIN DAN BERJALAN LANCAR

tambahan:

JANGAN LUPA BAHWA DUNIA SAAT INI TERHUBUNG OLEH KOMUNIKASI DATA YANG BEGITU CEPAT DAN PESAT DENGAN INTERNET. APAKAH PERLU PENGKAJIAN - PENINGKATAN - PENGADAAN SERTA PELATIHAN BAGI PEMBENTUKAN PASUKAN CYBER DI INTERNET ? 

SEBAGAI CONTOH : DRONE AMERIKA BERHASIL DITURUNKAN PAKSA OLEH  PASUKAN CYBER IRAN, KOMUNIKASI  DATA BISA DI HACK DAN DIKUASAI. DSB

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HAWK SPECIFICATIONS JET FIGHTER WITH NEW Self Protection RWR - MOST VIDEO REVIEW

Hawk RAF BAE Hawk T1 trainer Role Advanced trainer aircraft Manufacturer Hawker Siddeley (1974–1977) British Aerospace (1977–1999) BAE Systems MAS division First flight 21 August 1974 Introduction 1976 Status In service Primary users Royal Air Force Indian Air Force Finnish Air Force Royal Australian Air Force Produced 1974–present Number built 1,000+ Unit cost £18 million (2003) Variants British Aerospace Hawk 200 Developed into McDonnell Douglas T-45 Goshawk Specifications (Hawk 128) General characteristics Crew: 2: student, instructor Length: 12.43 m (40 ft 9 in) Wingspan: 9.94 m (32 ft 7 in) Height: 3.98 m (13 ft 1 in) Wing area: 16.70 m2 (179.64 ft2) Empty weight: 4,480 kg (9,880 lb) Useful load: 3,000 kg (6,600 lb) Max takeoff weight: 9,100 kg (20,000 lb) Powerplant: 1× Rolls-Royce Adour Mk. 951 turbofan with FADEC, 29 kN (6,500 lbf) 29 kN Performance Maximum speed: Mach 0.84 (1,028 km/h, 638 mph) at altitude Range: 2,520 km (1,360 nmi, 1,565 mi) Service ceiling: 13,565 m (44,500 ft) Rate of climb: 47 m/s (9,300 ft/min) Thrust/weight: 0.65 Armament Note: all armament is optional. 1× 30 mm ADEN cannon, in centreline pod Up to 6,800 lb (3,085 kg) of weapons on five hardpoints, including: 4× AIM-9 Sidewinder or ASRAAM on wing pylons and wingtip rails 1,500 lb (680 kg), limited to one centreline and two wing pylons (Hawk T1) wikipedia.org

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NEW RADAR TECHNOLOGY 
FOR HAWK 100/200 FAMILY
RWR Selex ES SEER Self Protection RWR Finmeccanica

FINMECCANICA – SELEX ES SEER SELF-PROTECTION SYSTEM IN ACTION DURING NATO TACTICAL LEADERSHIP PROGRAMME SEER demonstrated its ease of integration and high performance during the four-week exercise The system was integrated onto two Czech Air Force L-159 Advanced Light Combat Aircraft in under three hours   SEER identified air, land and sea-based threats at significant ranges with a high degree of accuracy, operating with 100% reliability during the exercise Finmeccanica – Selex ES demonstrated the ease of integration and consistent performance of its SEER digital Radar Warning Receiver (RWR) self-protection system during the recent NATO Tactical Leadership Programme (TLP) at Los Llanos Air Base, Albacete, Spain. The four-week exercise was held to increase the effectiveness of ten participating air forces.   The system was integrated onto two Czech Air Force AERO Vodochody AEROSPACE a.s. L-159 Advanced Light Combat Aircraft in under three hours, making use of the existing wiring and antennas that had previously serviced the legacy Finmeccanica – Selex ES’ Sky Guardian 200. This demonstrated the advantage of an open architecture approach and enabled the Czech Air Force to fully concentrate on planning and executing their flying programme. The L-159 installation was a case study in easily retrofitting an aircraft with next generation RWR capabilities. SEER performed precisely as expected during exercises and identified air, land and sea-based threats at significant ranges with a high degree of accuracy. Specialist Finmeccanica – Selex ES Electronic Warfare Operational Support (EWOS) staff provided the Czech Air Force with updated mission data files before each flight based on information and intelligence that had been gathered during the previous mission. This provided the pilots with a greater and more accurate picture of the threat environment enabling them to adapt to a variety of tasks during the programme.   Notes to editors SEER is an advanced digital Radar Warning Receiver (RWR). It is a self-protection equipment used to detect the radio-frequency signals of potentially hostile radars. The system is highly sensitive, providing detailed parametric and angle of arrival measurement of intercepted signals. SEER is fully programmable, allowing users to configure its operation with indigenous mission-dependent data. It is offered in E-J configuration with the ability to upgrade to C/D-K band capability. Its small-footprint, low-weight and power characteristics ensure its suitability for a range of new or upgrade programmes, including fixed and rotary wing aircraft and Unmanned Aerial Systems (UAS). finmeccanica.co.uk

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F-16 Fighting Falcon Specifications Jet Fighter Development History - Most Video Review

F-16 Fighting Falcon

F-16 Fighting Falcon A USAF F-16C over Iraq in 2008 Role Multirole fighter, air superiority fighter National origin United States Manufacturer General Dynamics Lockheed Martin Aeronautics First flight 20 January 1974 Introduction 17 August 1978 Status In service Primary users United States Air Force 25 other users (see operators page) Produced 1973–present Number built 4,540+[1] Unit cost F-16A/B: US$14.6 million (1998 dollars)[2] F-16C/D: US$18.8 million (1998 dollars)[2] Variants General Dynamics F-16 VISTA Developed into Vought Model 1600 General Dynamics F-16XL Mitsubishi F-2   Specifications (F-16C Block 50) General characteristics Crew: 1 Length: 49 ft 5 in (15.06 m) Wingspan: 32 ft 8 in (9.96 m) Height: 16 ft (4.88 m) Wing area: 300 ft² (27.87 m²) Airfoil: NACA 64A204 root and tip Empty weight: 18,900 lb (8,570 kg) Loaded weight: 26,500 lb (12,000 kg) Max. takeoff weight: 42,300 lb (19,200 kg) Powerplant: 1 × General Electric F110-GE-100 (for F-16C Block 50) afterburning turbofan Dry thrust: 17,155 lbf (76.3 kN) Thrust with afterburner: 28,600 lbf (127 kN) Performance Maximum speed: ** At sea level: Mach 1.2 (915 mph, 1,470 km/h)[66] At altitude: Mach 2[2] (1,320 mph, 2,120 km/h) clean configuration Combat radius: 340 mi (295 nmi, 550 km) on a hi-lo-hi mission with four 1,000 lb (450 kg) bombs Ferry range: 2,280 nmi (2,620 mi, 4,220 km) with drop tanks Service ceiling: 50,000+ ft[2] (15,240+ m) Rate of climb: 50,000 ft/min (254 m/s) Wing loading: 88.3 lb/ft² (431 kg/m²) Thrust/weight: 1.095 Maximum g-load: +9.0 g Armament Guns: 1 × 20 mm (0.787 in) M61A1 Vulcan 6-barrel Gatling cannon, 511 rounds Hardpoints: 2 × wing-tip Air-to-air missile launch rails, 6 × under-wing, and 3 × under-fuselage pylon (2 of 3 for sensors) stations with a capacity of Up to 17,000 lb (7,700 kg) of stores Rockets: **4 × LAU-61/LAU-68 rocket pods (each with 19/7 × Hydra 70 mm rockets, respectively) 4 × LAU-5003 rocket pods (each with 19 × CRV7 70 mm rockets) 4 × LAU-10 rocket pods (each with 4 × Zuni 127 mm rockets) Missiles: **Air-to-air missiles: 2 × AIM-7 Sparrow 6 × AIM-9 Sidewinder 6 × AIM-120 AMRAAM 6 × IRIS-T 6 × Python-4 Air-to-ground missiles: 6 × AGM-65 Maverick 4 × AGM-88 HARM AGM-158 Joint Air-to-Surface Standoff Missile (JASSM) Anti-ship missiles: 2 × AGM-84 Harpoon 4 × AGM-119 Penguin Bombs: 8 × CBU-87 Combined Effects Munition 8 × CBU-89 Gator mine 8 × CBU-97 Sensor Fuzed Weapon 4 × Mark 84 general-purpose bombs 8 × Mark 83 GP bombs 12 × Mark 82 GP bombs 8 × GBU-39 Small Diameter Bomb (SDB) 4 × GBU-10 Paveway II 6 × GBU-12 Paveway II 4 × GBU-24 Paveway III 4 × GBU-27 Paveway III 4 × Joint Direct Attack Munition (JDAM) series 4 × AGM-154 Joint Standoff Weapon (JSOW) Wind Corrected Munitions Dispenser (WCMD) B61 nuclear bomb B83 nuclear bomb Others: SUU-42A/A Flares/Infrared decoys dispenser pod and chaff pod or AN/ALQ-131 & AN/ALQ-184 ECM pods or LANTIRN, Lockheed Martin Sniper XR & LITENING targeting pods or Up to 3 × 300/330/370/600 US gallon Sargent Fletcher drop tanks for ferry flight/extended range/loitering time or UTC Aerospace DB-110 long range EO/IR sensor pod on centerline Avionics AN/APG-68 radar MIL-STD-1553 bus [231]  wikipedia.org

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T-50 Golden Eagle Specifications Jet Fighter - Most Video Review

T-50 Golden Eagle Republic of Korea Air Force TA-50 in 2010 Role Advanced trainer (T-50), Lead-in fighter trainer/Light combat aircraft (TA-50, FA-50) Manufacturer Korea Aerospace Industries (with technical support from Lockheed Martin) First flight 20 August 2002[1] Introduction 22 February 2005[2] Status In service Primary users Republic of Korea Air Force Indonesian Air Force Philippine Air Force Iraqi Air Force Produced 2001–present Number built 82 Unit cost T-50: US$21 million (2008)[3] TA-50: US$25 million (2011)[4] FA-50: US$30 million (2012)[5] General characteristics Crew: 2 Length: 13.14 m (43.1 ft) Wingspan: 9.45 m (31 ft) (with wingtip missiles) Height: 4.94 m (16.2 ft) Wing area: 23.69 m² (250 sqft) Empty weight: 6,470 kg (14,285 lb) Max. takeoff weight: 12,300 kg (27,300 lb) Powerplant: 1 × General Electric F404 (built under license by Samsung Techwin[17]) afterburning turbofan Dry thrust: 53.07 kN (11,925 lbf) Thrust with afterburner: 78.7 kN (17,700 lbf) Performance Maximum speed: Mach 1.5[43][138] (1,640 km/h, 1,020 mph at 9,144 m or 30,000 ft) Range: 1,851 km (1,150 mi) Service ceiling: 14,630 m (48,000 ft) Rate of climb: 198 m/s (39,000 ft/min) Thrust/weight: 0.96 Max g limit: -3 g / +8 g[43] Armament Guns: 1× 20 mm (0.787 in) General Dynamics A-50 3-barrel rotary cannon Hardpoints: Total of 7 with 4 underwing 2 wingtip and one under fuselage; holding up to 3,740 kg (8,250 lb) of payload Rockets: Hydra 70 LOGIR Missiles: Air-to-air: AIM-9 Sidewinder AIM-120 AMRAAM (planned for FA-50)[69] Air-to-ground: AGM-65 Maverick KEPD 350K-2 (planned for FA-50)[139][140] Bombs: Mk 82 Mk 83 CBU-97/105 Sensor Fuzed Weapon Spice-equipped bombs JDAM-equipped bombs WCMD Avionics AN/APG-67 (T-50) EL/M-2032 (TA-50 and FA-50) Lockheed Martin Advanced Avionics Note: armament for TA-50 and FA-50 only.

Spesifikasi T-50 dan perbandingannya

Produk		T-50 latih lanjut APT (Advanced Pilot Trainer)	TA-50 konversi pelatih FLI (Penerbangan-Lead-In)	FA-50 Serang Ringan	M-346, Italia APT
Karakteristik Operasi		rendahnya biaya perawatan operasional	kapasitas pelatihan taktis / harga pembuatan rendah	kemampuan misi malam	rendahnya biaya perawatan operasional
Spesifikasi	Produksi Selesai	25 unit 25/10 ( Black Eagles)	22	60 unit (22+38 dalam pembangunan)	dalam pengembangan
	Kru	2			2
	Panjang Pesawat	13.14m (43.1 ft)			11.49m (37.7 ft)
	Tinggi	4.94m (16.2 ft)			4.98m (16.33 ft)
	Lebar (dengan sayap)	9.45m (31.0 ft)			9.72m (31.9 ft)
	Kemiringan sayap utama	35 derajat (desain supersonik)			30 derajat (desain subsonik)
	Area sayap	23.69 m²			23.52m²
	Di antara kekosongan	6.454 ton			4.61 ton
	Berat Take-off minimum (bersih)	8,9 ton (2,45 + 6,454 = bahan bakar internal)			6.7 ton
	Maksimum berat lepas landas	13,5 ton (4,53 + 8,9 = bersenjata)			9.5 ton
	Bahan Bakar Internal	2.5 ton			2 ton
	Mesin	General Electric F404-GE-102			F-124GA-200 * 2 (kembar)
	Dorongan	8.04 ton			5.7 ton (2.85*2)
Kinerja	kecepatan maximum	Mach 1.5+			590 KTS (mach 0.9)
	Toleransi percepatan gravitasi	-3 ~ +8.3G (gravitasi putaran 6.5G)			-3~8G(15000ft gravitasi konstan di 5.8G)
	Waktu menanjak	14.5 detik / 15,000 ft (grafik E-M), mendekati F-16			14 detik / 15000 ft
	Daya tanjak	12070 m /menit			6100 m/menit
	ketinggian maksimum	14.8km (48,500ft) / 55,000ft dengan afterburner			13.715km (45000ft) / tanpa afterburner
	Kecepatan Stall	105KTS (195km/h) - A-10= 220km/h			90KTS (167km/h)
	Jarak roll Lepas landas / mendarat	345m / 707m			320m / bahan bakar internal 470m (20 %)
	Daya jelajah	1400km (bahan bakar internal, tidak bersenjata), Radius misi 444km (230nm, tangki bahan bakar internal + AIM-9 (2) + AGM65 (2))			1120nm (bahan bakar internal, tidak bersenjata)
Persenjataan	Tangki eksternal	150 gal*3		300 gal*3	153 gal*3
	Kanon	Bersenjata	internal 20 mm (205 peluru)
	Roket
	Rudal		AIM-9 / ACMI 2 kaki	AIM-9L (rudal jarak pendek)	Pendek / Menengah
	Untuk rudal-darat		AGM-65 g Maverick 4 pylon (A-10)
	Bom		bom berpandu laser (GBU-12 Paveway 2) 8 pylon	JDAM (2000 lbs) 3 pylon	1.000 lbs atau kurang
	Radar		APG-67 (v) 4> berubah ke EL/M-2032	EL/M-2032	Cellex-C AESA vixen 500E(optional)
	Poin Bersenjata		7 lokasi (350 lbs*2/1600 lbs*2/2700 lbs*3)	7 lokasi	2 (optonal)
	Muatan eksternal maksimum		10.000 lbs (9750 lbs untuk memverifikasi atau 4,53 ton)	12.000 lbs (desain beban yang diperbolehkan 20.000 lbs)	2.8 ton

wikipedia.org

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