Predloga:Specifikacije letala/testniprimeri

Fairchild Republic A-10 Thunderbolt II

Podatki iz The Great Book of Modern Warplanes,^[1] Fairchild-Republic A/OA-10,^[2] USAF^[3]

Splošne karakteristike

Posadka: 1
Dolžina: 53 ft 4 in (16,26 m)
Razpon kril: 57 ft 6 in (17,53 m)
Višina: 14 ft 8 in (4,47 m)
Površina kril: 506 ft² (47,0 m²)
Aeroprofil: NACA 6716 root, NACA 6713 tip
Teža praznega letala: 24.959 lb (11.321 kg)
Naložena teža: 30.384 lb (13.782 kg)
CAS mission: 47.094 lb (21.361 kg)
Anti-armor mission: 42.071 lb (19.083 kg)
Maks. vzletna teža: 50.000 lb (23.000 kg)
Pogon letala: 2 × General Electric TF34-GE-100A turbofans, 9.065 lbf (40,32 kN) each
Internal fuel capacity: 11.000 lb (4.990 kg)

Zmogljivost

Neprekoračljiva hitrost: 450 knots (518 mph,^[2] 833 km/h) at 5,000 ft (1,500 m) with 18 Mk 82 bombs^[4]
Maks. hitrost: 381 knots (439 mph, 706 km/h) at sea level, clean^[2]
Potovalna hitrost: 300 knots (340 mph, 560 km/h)
Hitrost pri porušitvi vzgona: 120 knots (138 mph, 220 km/h) ^[5]
Combat radius:
- CAS mission: 250 nmi (288 mi, 460 km) at 1.88 hour loiter at 5.000 ft (1.500 m), 10 min combat
- Anti-armor mission: 252 nmi (290 mi, 467 km), 40 nmi (45 mi, 75 km)) sea-level penetration and exit, 30 min combat
Največji doseg: 2.240 nmi (2.580 mi, 4.150 km) with 50 knot (55 mph, 90 km/h) headwinds, 20 minutes reserve
Višina leta: 45.000 ft (13.700 m)
Hitrost vzpenjanja: 6,000 ft/min (30 m/s)
Obremenitev kril: 99 lb/ft² (482 kg/m²)
Razmerje potisk/teža: 0,36

Oborožitev

Strelno orožje: 1× 30 mm (1,18 in) GAU-8/A Avenger Gatling cannon with 1.174 rounds (Capacity 1,350)
Nosilci za orožje: 11 (8× under-wing and 3× under-fuselage pylon stations) s kapaciteto 16.000 lb (7.260 kg) and provisions to carry combinations of:
- Rakete:
  - 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)
  - 6× LAU-10 rocket pods (each with 4× 127 mm (5.0 in) Zuni rockets)
- Izstrelki:
  - 2× AIM-9 Sidewinders air-to-air missiles for self-defense
  - 6× AGM-65 Maverick air-to-surface missiles
- Bombe:
  - Mark 80 series of unguided iron bombs or
  - Mk 77 incendiary bombs or
  - BLU-1, BLU-27/B Rockeye II, Mk20, BL-755^[6] and CBU-52/58/71/87/89/97 cluster bombs or
  - Paveway series of Laser-guided bombs or
  - Joint Direct Attack Munition (A-10C)^[7] or
  - Wind Corrected Munitions Dispenser (A-10C)
- Drugo:
  - SUU-42A/A Flares/Infrared decoys and chaff dispenser pod or
  - AN/ALQ-131 or AN/ALQ-184 ECM pods or
  - Lockheed Martin Sniper XR or LITENING targeting pods (A-10C) or
  - 2× 600 US gallon Sargent Fletcher drop tanks for increased range/loitering time.

Letalska elektronika

AN/AAS-35(V) Pave Penny laser tracker pod^[8] (mounted beneath right side of cockpit) for use with Paveway LGBs
Head-up display (HUD) for improved technical flying and air-to-ground support.^[9]

Bell 206

Podatki iz Bell 206B-L4 specifications^[10]^[11]

Splošne karakteristike

Posadka: one pilot
Število sedežev: four passengers
Dolžina: 39 ft 8 in (12,11 m)
Premer rotorja: 33 ft 4 in (10,16 m)
Višina: 9 ft 4 in (2,83 m)
Površina rotorjev: 872 ft² (81,1 m²)
Teža praznega letala: 2.331 lb (1.057 kg)
Maks. vzletna teža: 3.200 lb (1.451 kg)
Pogon letala: 1 × Allison 250-C20B turboshaft, 420 shp; derated to 317 shp due to drivetrain limitations (310 kW)

Zmogljivost

Neprekoračljiva hitrost: 130 knots (241 km/h, 150 mph)
Maks. hitrost: 120 knots (222 km/h, 138 mph)
Doseg: 374 nmi (430 mi, 693 km)
Višina leta: 13.500 ft (4.115 m)
Hitrost vzpenjanja: 1.350 ft/min (6,9 m/s)
Obremenitev rotorja: 4 lb/ft² (177 N/m²)
Razmerje moč/teža: 0,26 hp/lb (427,48784 W/kg)

ref dump

↑ Spick 2000, pp. 21, 44–48.
↑ ^2,0 ^2,1 ^2,2 Jenkins 1998, p. 54.
↑ Napaka pri navajanju: Neveljavna oznaka <ref>; sklici, poimenovani USAF_factsh, ne vsebujejo besedila (glej stran pomoči).
↑ Flight manual TO 1A-10A-1 (20 February 2003, Change 8), pp. 5–24.
↑ Aalbers, Willem "Palerider". "History of the Fairchild-Republic A-10 Thunderbolt II, Part Two." Simhq.com. Retrieved: 5 March 2010.
↑ Flight Manual TO 1A-10A-1 (20 February 2003, Change 8), pp. 5–30.
↑ Pike, John. "A-10 Specs." Global Security. Retrieved: 5 March 2010.
↑ "Lockheed Martin AN/AAS-35(V) Pave Penny laser tracker." Jane's Electro-Optic Systems, 5 January 2009. Retrieved: 5 March 2010.
↑ "A-10 vs F-16: Go Ugly Early, HUD Video." Liveleak.com, 24 January 2009. Retrieved: 5 March 2010.
↑ »Bell 206 L4 Product Specifications« (PDF). Bell Helicopter. Februar 2013. Pridobljeno 16. junija 2013.
↑ »Bell 206 L4 specifications« (PDF). Bell Helicopter. Pridobljeno 16. junija 2013.

Specifikacije(MiG-25P)

Podatki iz The Great Book of Fighters,^[1]^{[navedi št.strani]} International Directory of Military Aircraft,^[2] Combat Aircraft since 1945^[3]

Splošne karakteristike

Posadka: One
Dolžina: 19.75 m (64 ft 10 in)
Razpon kril: 14.01 m (45 ft 11.5 in)
Višina: 6.10 m (20 ft 0.25 in)
Površina kril: 61.40 m² (660.93 ft²)
Teža praznega letala: 20,000 kg (44,080 lb)
Naložena teža: 36,720 kg (80,952 lb)
Pogon letala: 2 × Tumansky R-15B-300 afterburning turbojets
- Potisk motorjev (suh): 73.5 kN (16,524 lbf) vsak
- Potisk motorjev z dodatnim zgorevanjem: 100.1 kN (22,494 lbf) vsak

Zmogljivost

Maks. hitrost:
- High altitude: Mach 3.2^[4] (3,470 km/h, 2,170 mph); Mach 2.83 (3,200 km/h, 1,920 mph) continuous engine limit^[4]
- Low altitude: 1,200 km/h (648 knots, 746 mph) at altitude^[2]
Doseg: 1,730 km (935 nmi, 1,075 mi) with internal fuel
Največji doseg: 2,575 km (1,390 nmi)
Višina leta: 20,700 m (67,915 ft) with four missiles; over 24,400 m (80,000 ft) for RB models
Hitrost vzpenjanja: 208 m/s (40,950 ft/min)
Obremenitev kril: 598 kg/m² (122.5 lb/ft²)
Razmerje potisk/teža: 0.41
Time to altitude: 8.9 min to 20,000 m (65,615 ft)

Oborožitev

2x radar-guided R-40R (AA-6 "Acrid") air-to-air missiles, and

2x infrared-guided R-40T missiles

Letalska elektronika

RP-25 Smerch radar
A RV-UM or a RV-4 radar altimeter

Specifikacije Cessna (172R)

Podatki iz Cessna^[5]^[6]

Splošne značilnosti

Posadka: one
Število sedežev: three passengers
Dolžina: 27 ft 2 in (8,28 m)
Razpon kril: 36 ft 1 in (11,00 m)
Višina: 8 ft 11 in (2,72 m)
Površina kril: 174 sq ft (16,2 m²)
Vitkost: 7.32
Aeroprofil: modified NACA 2412
Teža praznega letala: 1.691 lb (767 kg)
Bruto teža: 2.450 lb (1.111 kg)
Kapaciteta goriva: 56 US gallons (212 litres)
Pogon letala: 1 × Lycoming IO-360-L2A four cylinder, horizontally opposed aircraft engine, 160 hp (120 kW)
Propelerji: št. lopatic: 2 metal

Zmogljivost

Potovalna hitrost: 122 kn (140 mph; 226 km/h)
Hitrost pri porušitvi vzgona: 47 kn (54 mph; 87 km/h) (power off, flaps down)^[7]
Neprekoračljiva hitrost: 163 kn (188 mph; 302 km/h) (IAS)^[8]
Doseg: 696 nmi (801 mi; 1.289 km) with 45 minute reserve, 55% Power, at 12,000 ft
Višina leta (servisna): 13.500 ft (4.100 m)
Hitrost vzpenjanja: 721 ft/min (3,66 m/s)
Obremenitev krila: 141 lb/sq ft (686 kg/m²)

Letalska elektronika

Optional Garmin G1000 Primary Flight Display

↑ Green and Swanborough 2001.
↑ ^2,0 ^2,1 Frawley 2002, p. 123.
↑ Wilson 2000, p. 103.
↑ ^4,0 ^4,1 Napaka pri navajanju: Neveljavna oznaka <ref>; sklici, poimenovani Great Book, ne vsebujejo besedila (glej stran pomoči).
↑ Cessna (2009). »Cessna Skyhawk Performance«. Pridobljeno 22. avgusta 2010.
↑ Cessna (Maj 2010). »Skyhawk 172R Specification and Description« (PDF). Pridobljeno 22. avgusta 2010.
↑ Jackson 2003, pp. 588–589.
↑ Napaka pri navajanju: Neveljavna oznaka <ref>; sklici, poimenovani 3A12, ne vsebujejo besedila (glej stran pomoči).

[1] Spick 2000, pp. 21, 44–48.

[Jenkins_p54-2] 2,0 ^2,1 ^2,2 Jenkins 1998, p. 54.

[USAF_factsh-3] Napaka pri navajanju: Neveljavna oznaka <ref>; sklici, poimenovani USAF_factsh, ne vsebujejo besedila (glej stran pomoči).

[4] Flight manual TO 1A-10A-1 (20 February 2003, Change 8), pp. 5–24.

[5] Aalbers, Willem "Palerider". "History of the Fairchild-Republic A-10 Thunderbolt II, Part Two." Simhq.com. Retrieved: 5 March 2010.

[6] Flight Manual TO 1A-10A-1 (20 February 2003, Change 8), pp. 5–30.

[GS_SPECS-7] Pike, John. "A-10 Specs." Global Security. Retrieved: 5 March 2010.

[8] "Lockheed Martin AN/AAS-35(V) Pave Penny laser tracker." Jane's Electro-Optic Systems, 5 January 2009. Retrieved: 5 March 2010.

[Ugly-9] "A-10 vs F-16: Go Ugly Early, HUD Video." Liveleak.com, 24 January 2009. Retrieved: 5 March 2010.

[10] »Bell 206 L4 Product Specifications« (PDF). Bell Helicopter. Februar 2013. Pridobljeno 16. junija 2013.

[11] »Bell 206 L4 specifications« (PDF). Bell Helicopter. Pridobljeno 16. junija 2013.

[12] Green and Swanborough 2001.

[Frawley-13] 2,0 ^2,1 Frawley 2002, p. 123.

[Wilson-14] Wilson 2000, p. 103.

[Great_Book-15] 4,0 ^4,1 Napaka pri navajanju: Neveljavna oznaka <ref>; sklici, poimenovani Great Book, ne vsebujejo besedila (glej stran pomoči).

[172RSpecs-16] Cessna (2009). »Cessna Skyhawk Performance«. Pridobljeno 22. avgusta 2010.

[SpecPDF-17] Cessna (Maj 2010). »Skyhawk 172R Specification and Description« (PDF). Pridobljeno 22. avgusta 2010.

[JAWA03_p588–9-18] Jackson 2003, pp. 588–589.

[3A12-19] Napaka pri navajanju: Neveljavna oznaka <ref>; sklici, poimenovani 3A12, ne vsebujejo besedila (glej stran pomoči).

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