especificaciones aviones chuck yeager

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P-51D Mustang

Data from Erection and Maintenance Manual for P-51D and P-51K.[69]

The Great

Book of Fighters,[70]

and Quest for Performance[71]

Gener al char acteristics

Crew: 1

Length: 32 ft 3 in (9.83 m) Wingspan: 37 ft 0 in (11.28 m)

Height: 13 ft 4½ in (4.08 m:tail wheel on ground, vertical propeller blade.)

Wing area: 235 ft² (21.83 m²)

Empty weight: 7,635 lb (3,465 kg)

Loaded weight: 9,200 lb (4,175 kg)

Max takeoff weight: 12,100 lb (5,490 kg)

Power plant: 1× Packard V-1650-7 liquid-cooled supercharged V-12,

1,490 hp (1,111 kW) at 3,000 rpm;[72]

1,720 hp (1,282 kW) at WEP

Zer o-lif t dr ag coeff icient: 0.0163

Dr ag area: 3.80 ft² (0.35 m²)

Aspect r atio: 5.83

Per for mance

Maximum speed: 437 mph (703 km/h) at 25,000 ft (7,600 m)



Specif ications (F-86F-40-NA)

Data from The North American Sabre[64]


Crew: 1

Length: 37 ft 1 in (11.4 m)

Wingspan: 37 ft 0 in (11.3 m)

Height: 14 ft 1 in (4.5 m) Wing area: 313.4 sq ft (29.11 m²)




Power plant: 1 × General Electric J47-GE-27 turbojet,

5,910 lbf (ma imum thrust at 7.950 rpm for five min) (26.3 kN)

Fuel pr ovisions Internal fuel load: 437 gallons (1,650 l), Drop

tanks: 2 200 gallons (756 l) JP-4 fuel

Per for mance

Maximum speed: 687 mph (1,106 km/h) at sea level at 14,212 lb

(6,447 kg) combat weight

also reported 678 mph (1,091 km/h) and 599 at 35,000 feet

(11,000 m) at 15,352 pounds (6,960 kg). (597 knots, 1,105 km/h

at 6446 m, 1,091 and 964 km/h at 6,960 m.)



Ar mament

Guns: 2 × 13 mm (.51 in) MG 131 machine guns with 475 rpg

2 × 20 mm MG 151 cannons with 250 rpg in the wing root

Bom s: 1 × 500 kg (1,102 lb) S 500 bomb (optional)

Specif ications (MiG-15bis)

MiG-15 TI



Mi -15 rawing

Gener al char acter istics

Cr ew: Mi -15bis=1, Mi -15U I=2

Length: 10.11 m ft 2 in) Wingspan: 10.08 m ft 1 in)

Height: . 0 m 12 ft 2 in)

Wing ar ea: 20. m² 221. ft²)

Air foil: s A I S-10 / s A I SR -3

Empty weight: 3,580 kg , 00 lb)

Loaded weight: , 0 kg 10, 35 lb)

Max takeoff weight: ,105 kg 13, 0 lb)

Fuel capacity: 1, 00 L 364 US gal)

Power plant: 1 Klimov VK-1 turbo jet, 26.5 kN 5, 50 lbf )

Per for mance

Maximum speed: 1,075 km/h 668 mph)

Cruise speed: 840 km/h 520 mph)

Range: 1,200 km, 1, 75 km with external tanks 745 mi / 1,225

mi)

Service ceiling: 15,500 m 50,850 ft) Rate of climb: 50 m/s ,840 ft/min)

Wing loading: 240.8 kg/m² 49.3 lb/ft²)

Thrust /weight: 0.54

Ar mament

2x NR-23 23mm cannons in lower left f uselage 80 rounds per

gun, 160 rounds total)

1x Nudelman N-37 37 mm cannon in lower r ight f uselage 40

rounds total)

2x 100 kg 220 lb) bombs, drop tanks, or unguided rockets on 2

underwing hardpoints.

[edit]



Specif ications (Mikoyan-Gurevich MiG-21F-13)

(Specifications for other models can be found at:-Miko an-Gurevich

MiG-21 variants)

Data from [1]


Crew: 1

Length: 15.76 (with pitot tube) m (51 ft 8.47 in)

Wingspan: 7.154 m (23 ft 5.66 in)

Height: 4.1 m (13 ft 5.41 in)

Wing area: 23.0 m² (247.3 ft²)

Empty weight: 4,871 kg (10,738 lb)

Gr oss weight: 7,100 kg (15,650 lb)

Power plant: 1 × Tumansk 11F-300, 37.27 kN (8,380 lbf)

thrust dr , 56.27 kN (12,650 lbf) with afterburner each

Per for mance

Maximum speed: 2,125 km/h (1,385 mph)

Maximum speed: Mach 2.05

Range: 1,580 km (981 miles)

Ser vice ceiling: 19,000 m (62,335 ft)



Ar mament

1x internal 30 mm NR-30 cannon, plus

2x K-13 or K-13 A R-3S) AAM or

2x 500 kg 1,102 lbs) of bombs

Specifications Bf 109 -6)

Dat a f rom he reat Book of ighters[71]

and the Fi 7 7

is8

Ai r F orce Bf 109 M anual


Cr ew: One

Length: 8.95 m 29 ft 7 in)

Wingspan: 9.925 m 32 ft 6 in)

Height: 2.60 m 8 ft 2 in)

Wing ar ea: 16.05 m² 173.3 ft²)

Empty weight: 2,247 kg 5,893 lb)

Loaded weight: 3,148 kg 6,940 lb)

Max takeoff weight: 3,400 kg 7,495 lb)

Power plant: 1× aimler-Benz B 605 A-1 li uid-cooled inver ted V12,

1,475 PS 1,455 hp, 1,085 kW)

Pr opeller s: V M 9-12087 three-bladed light-alloy propeller



Pr opeller diameter : 3 m 9.84 ft) )

Per for mance

Maximum speed: 640 km/h 398 mph) at 6,300 m 20,669 ft)

Cruise speed: 590 km/h 365 mph) at 6,000 m 19,680 ft) Range: 850 km 528 mi) 1,000 km 621 mi) with droptank

Service ceiling: 12,000 m 39,370 ft)

Rate of climb: 17.0 m/s 3,345 ft/min)

Wing loading: 196 kg/m² 40 lb/ft²)

Power/mass: 344 W/kg 0.21 hp/lb)

Ar mament

Guns:

2 × 13 mm .51 in) MG 131 machine guns with 300 rounds per gun

1 × 20 mm MG 151 cannon as Motorkanone with 150 rpg. G-6/U4

var iant: 1 × 30 mm 1.18 in) MK 108 cannon as M ot or k anone with 65

rpg

2 × 20 mm MG 151/20 underwing cannon pods with 135 rpg optional

kit - Rüstsatz VI)

Rockets: 2 × 21 cm 8 in) Wf r . Gr . 21 rockets G-6 with BR21)

Bombs: 1 × 250 kg 551 lb) bomb or 4 × 50 kg 110 lb) bombs or 1 ×

300 litres 79 USgal)

Specifications Messerschmitt Bf 110 C-4)

Dat a f rom[c it ati on need ed ]


Cr ew: 2 3 f or night fighter var iants)

Length: 12.3 m 40 ft 6 in)



Wing ar ea: 38.8 m² 414 ft²)





Power plant: 2× aimler-Benz B 601B-1 li uid-cooled inver ted V-12, 809

kW 1,085 hp)1,100 PS each

Per for mance

Maximum speed: 560 km/h 348 mph)

Range: 2,410 km 1,500 mi)

Ferr y r ange: 2,800 km 1,750 mi)


Wing loading: 173 kg/m² 35.7 lb/ft²)

Power/mass: 0.3644 kW/kg 0.155 hp/lb)

Ar mament

Guns:

2 × 20 mm MG /M cannons 180 rpg - 3 drums with 60 rpg, cannon were reloaded by rear gunner or radio operator dur ing flight)

4 × 7.92 mm .312 in) MG 17 machine guns 1,000 rpg)

1 × 7.92 mm .312 in) MG 15 machine guns f or def ense

[edit]Specifications Messerschmitt Bf 110 G-2)

Dat a f rom f rom M esser schmitt BF 110/M e 210/M e 410: An Ill ust r at ed Hist or y


Cr ew: 2 3 f or night fighter var iants) Length: 12.3 m 40 ft 6 in)



Wing ar ea: 38.8 m² 414 ft²)


Power plant: 2× aimler-Benz B 605B li uid-cooled inver ted V-12, 1,085

kW 1,455 HP)1,475 PS each

Per for mance

Maximum speed: 595 km/h 370 mph)

Range: 900 km 558 mi) ; 1,300 km 807 mi) with droptanks


Rate of climb: 8 min to 6,000 m 20,000 ft)

Wing loading: max. 243 kg/m² )



Ar mament

Guns:

2 × 20 mm MG 151 cannons 750 rounds: 350 rpg + 400 rpg rounds

4 × 7.92 mm .312 in) MG 17 machine guns with 1,000 rounds per gun

1 × 7.92 mm .312 in) MG 81Z twin machine gun installation in rear

cockpit, with 850 rounds per gun

[edit] Specifications: Me 163 B-1


Cr ew: 1 Length: 5.70 m 18 ft 8 in)



Wing ar ea: 18.5 m² 200 ft²)




Power plant: 1 × Walter HWK 109-509 A-2 li uid-f uel rocket, 17 kN 3,800

lbf )

Per for mance

Maximum speed: 1,060 km/h 596 mph)

Range: 40 km 25 mi)


Rate of climb: 160 m/s[34]

[N 5]

31500 ft/min)

Wing loading: 213 kg/m² 43 lb/ft²)


Ar mament

Guns: *2 × 30 mm 1.18 in) Rheinmetall Borsig MK 108 cannons 60 rpg)

[edit]



Power plant: 1× Pratt & Whitne -2800-59 twin-row radial engine, 2,535

hp (1,890 kW)

Per for mance

Maximum speed: 433 mph at 30,000 ft (697 km/h at 9,145 m) Range: 800 mi combat, 1,800 mi ferr (1,290 km / 2,900 km)

Ser vice ceiling: 43,000 ft (13,100 m)

Rate of clim : 3,120 ft/min (15.9 m/s)

Wing loading: 58.3 lb/ft² (284.8 kg/m²)

Power /mass: 0.14 hp/lb (238 W/kg)

Ar mament

8 × .50 in (12.7 mm) M2 Browning machine guns (3400 rounds)

p to 2,500 lb (1,134 kg) of bombs

10 × 5 in (130 mm) unguided rockets

Specifications (Yak-9D)

Yak-9P




Cr ew: one

Length: 28 ft 0 in 8.55 m)

Wingspan: 31 ft 11 in 9.74 m)

Height: 9 ft 10 in 3.00 m)

Wing ar ea: 185.1 ft² 17.2 m²)

Empty weight: 5,170 lb 2,350 kg)

Loaded weight: 6,858 lb 3,117 kg)

Max takeoff weight: lb kg)

Power plant: 1× Klimov M-105 P V-12 li uid-cooled piston engine, 1,180

hp 880 kW)

Per for mance

Maximum speed: 367 mph at altitude 591 km/h)

Range: 845 miles 1,360 km)

Service ceiling: 30,000 ft 9,100 m)

Rate of climb: 2,690 ft/min 13.7 m/s)

Wing loading: 37 lb/ft² 181 kg/m²)

Power/mass: 0.17 hp/lb 0.28 kW/kg)

Ar mament

1 × 20 mm ShVAK cannon, 120 rounds

1 × 12.7 mm UBS machine gun, 200 rounds

[edit]Specifications Yak-9U VK-107))


Cr ew: one

Length: 28 ft 0 in 8.55 m)


Height: 9 ft 10 in 3.00 m) Wing ar ea: 185.1 ft² 17.2 m²)



Max takeoff weight: lb kg)

Power plant: 1× Klimov VK-107 A V-12 li uid-cooled piston engine, 1,500 hp

1,120 kW)



Per for mance

Maximum speed: 417 mph at altitude 672 km/h)

Range: 420 miles 675 km)




Power/mass: 0.21 hp/lb 0.35 kW/kg)

Ar mament

1 × 20 mm ShVAK cannon, 120 rounds

2 × 12.7 mm UBS machine guns, 170 rpg

[edit] Specifications MiG-17F)

Bluepr ints:[1]

Dat a f rom MiG: Fifty Years of Secret Aircraft esign[24]


Cr ew: One

Length: 11.26 m 36 ft 11½ in)


Height: 3.80 m 12 ft 5½ in)

Wing ar ea: 22.6 m² 243.3 ft²)

Empty weight: 3,919 kg[25] 8,640 lb)



Power plant: 1 × Klimov VK-1F afterburning turbo jet

Dr y thrust: 22.5 kN 5,046 lbf )

Thrust with af ter bur ner : 33.8 kN 7,423 lbf )

Per for mance

Maximum speed: 1,145 km/h 618 knots, 711 mph) at 3,000 m 10,000 ft)

Range: 2,020 km 1,091 nmi, 1,255 mi) with drop tanks


Rate of climb: 65 m/s 12,800 ft/min)

Ar mament



1 37 mm Nudelman N-37 cannon (40 rounds total)

2 23 mm Nudelman- ikhter N -23 cannons (80 rounds per gun, 160

rounds total)

p to 500 kg (1,100 lb) of e ternal stores on two p lons, including 100 kg

(220 lb) and 250 kg (550 lb) bombs, unguided rockets or e ternal fuel tanks.[edit]

Specifications (F-105D)

A surviving F-105D Thunderchief at theNational Museum of the 9 nited States Air Force.

Data from The Great Book of Fighters[4]

an@

Quest for Performance[22]


Crew: 1 (2 for F-105 /E/F/G variants)

Payload: 14,000 lb (6,700 kg) of weapons

Length: 64 ft 4.75 in (19.63 m)

Wingspan: 34 ft 11.25 in (10.65 m)

Height: 19 ft 8 in (5.99 m)



Wing ar ea: 385 ft² 35.76 m²)

Air foil: N ACA 65 A005.5 root, N ACA 65 A003.7 tip



Max takeoff weight: 52,546 lb 23,834 kg) Power plant: 1 × Pratt & Whitney 75-P-19W afterburning turbo jet

Dr y thrust: 14,300 Ibf 63,74kN)

Thrust with af ter bur ner : 24,500 Ibf 109 kN)


Dr ag ar ea: 6.65 ft² 0.62 m²)

Aspect r atio: 3.16

Per for mance

Maximum speed: Mach 2.08 1,372 mph, 2,208 km/h) at 36,000 ft

11,000 m)

Combat r adius: 780 mi 680 nmi, 1,250 km)

Ferr y r ange: 2,210 mi 1,920 nmi, 3,550 km)


Rate of climb: 38,500 ft/min 195 m/s)



Lif t-to-dr ag r atio: 10.4 Time to altitude: 1.7 min to 35,000 ft 11,000 m)

Ar mament

Guns: 1× 20 mm 0.787 in) M61 Vulcan 6-barreled gatling cannon, 1,028

rounds

Har dpoints: 5 total: 4× under-wing, 1× center line pylon stations plus an

internal bomb bay with a capacity of Up to 14,000 lb 6,400 kg) of

ordnance, including conventional and nuclear bombs, and AIM-9

Sidewinder and AGM-12 Bullpup missiles.



Specif ications (B-17G)

Data from The Enc clopedia of World Aircraft [32]


Crew: 10: Pilot, co-pilot, navigator, bombardier/nose gunner, flight engineer -

top turret gunner, radio operator, waist gunners (2), ball turret gunner, tail

gunner [161]

Length: 74 ft 4 in (22.66 m)

Wingspan: 103 ft 9 in (31.62 m) Height: 19 ft 1 in (5.82 m)

Wing area: 1,420 sq ft (131.92 m2)

Air foil: NA A 0018 / NA A 0010

Aspect r atio: 7.57




Power plant: 4× Wright -1820-97 " clone" turbosupercharged radial

engines, 1,200 hp (895 kW) each

Per for mance

Maximum speed: 287 mph (249 kn, 462 km/h)

Cr uise speed: 182 mph (158 kn, 293 km/h)

Range: 2,000 mi (1,738 nmi, 3,219 km) with 2,700 kg (6,000 lb) bombload



Ser vice ceiling: 35,600 ft (10,850 m)

Rate of clim : 900 ft/min (4.6 m/s)

Wing loading: 38.0 lb/sq ft (185.7 kg/m2)

Power /mass: 0.089 hp/lb (150 W/kg)

Ar mament

Guns: 13 × .50 in (12.7 mm) M2 Browning machine guns in 4 turrets in

dorsal, ventral, nose and tail, 2 in waist positions, 2 beside cockpit and 1 in

the lower dorsal position

Bom s:

Shor t r ange missions (<400 mi): 8,000 lb (3,600 kg)

Long r ange missions (§800 mi): 4,500 lb (2,000 kg)

Over load: 17,600 lb (7,800 kg)

[edit]

Specifications (B-29)

Boeing B-29 Superfortress

Data from Quest for Performance[56]


Crew: 11 (5 officers, 6 enlisted): (A/ )Airplane ommander , Pilot, flight

engineer (a rated pilot), [57][58]bombardier , navigator , radio operator, radar

operator, blister gunners (two), F upper gunner, and tail gunner

Length: 99 ft 0 in (30.18 m)

Wingspan: 141 ft 3 in (43.06 m)

Height: 29 ft 7 in (8.5 m)

Wing area: 1,736 sq ft (161.3 m²)





Max takeoff weight: 133,500 lb 60,560 kg) ; 135,000 lb plus combat load

155,000 lb on record)[41]

Power plant: 4× Wr ight R-3350-23 and 23 A turbosupercharged radial

engines, 2,200 hp 1,640 kW) each


Dr ag ar ea: 41.16 ft² 3.82 m²)

Aspect r atio: 11.50

Per for mance

Maximum speed: 357 mph 310 knots, 574 km/h)

Cruise speed: 220 mph 190 knots, 350 km/h) Stall speed: 105 mph 91 knots, 170 km/h)

Combat r ange: 3,250 mi 2,820 nmi, 5,230 km)

Ferr y r ange: 5,600 mi 4,900 nmi, 9,000 km, record 7,916 miles, 12,740

km)[40]

)


Rate of climb: 900 ft/min 4.6 m/s)

Wing loading: 69.12 lb/sqft 337 kg/m²)

Power/mass: 0.073 hp/lb 121 W/kg)

Lif t-to-dr ag r atio: 16.8

Ar mament

Guns:

8× .50 in 12.7 mm) caliber Browning M2/ANs in remote controlled

turrets[59].

2× .50 in and 1× 20 mm M2 cannon in tail position the cannon was

eventually removed as it proved unreliable in service )

B-29B-BW ± All armament and sighting equipment removed except f or

tail position; initially 2 x .50 in M2/AN and 1× 20 mm M2 cannon, later 3 x

2 x .50 in M2/AN with APG-15 gun-laying radar fitted as standard.

Bombs: 20,000 lb 9,000 kg) standard loadout



Specifications (B-52 )

B-52 A profile

Boeing B-52 A static displaB

with weapons, Barksdale AFB 2006

Data from Knaack,[201] SAF fact sheet,[1] Quest for Performance[202]


Crew: 5 (pilot, copilot, radar navigator (bombardier) , navigator ,

and Electronic Warfare fficer )

Length: 159 ft 4 in (48.5 m)




Height: 40 ft 8 in 12.4 m)

Wing ar ea: 4,000 sqft 370 m²)

Air foil: N ACA 63 A219.3 mod root, N ACA 65 A209.5 tip

Empty weight: 185,000 lb 83,250 kg) Loaded weight: 265,000 lb 120,000 kg)

Max takeoff weight: 488,000 lb 220,000 kg)

Power plant: 8 × Pratt & Whitney F33-P-3/103 turbof ans, 17,000 lbf 76

kN) each

Fuel capacity: 47,975 U.S. gal 39,948 imp gal; 181,610 L)

Zer o-lif t dr ag coeff icient: 0.0119 estimated)

Dr ag ar ea: 47.60 sqft 4.42 m²)

Aspect r atio: 8.56

Per for mance

Maximum speed: 560 kt 650 mph, 1,047 km/h)

Combat r adius: 4,480 mi 3,890 NM, 7,210 km)

Ferr y r ange: 10,145 mi 8,764 nm, 16,232 km)




Thrust /weight: 0.31 Lif t-to-dr ag r atio: 21.5 estimated)

Ar mament

Guns: 1× 20 mm 0.787 in) M61 Vulcan cannon or iginally mounted in a

remote controlled tail turret on the H -model, removed f rom all current

operational aircraft in 1991

Bombs: Approximately 70,000 pounds 31,500 kg) mixed ordnance;

bombs, mines, missiles, in var ious configurations

Avionics

Electro-optical viewing system that uses platinum silicide f orward-

looking inf rared and high resolution low-light-level television sensors

Sniper Advanced argeting Pod[203



Specifications L-5)

Dat a f rom March Field Air Museum web site [3]


Cr ew: 2 pilot and observer)

Length: 24 ft 1 in 7.34m)

Wingspan: 34ft 0 in 10.36m)

Height: 7 ft 11 in 2.41m)

Wing ar ea: 155 ft² 14.40m²)

Empty weight: 1550 lb 702kg)

Loaded weight: 2020 lb 916kg)

Usef ul load: lb kg)

Max takeoff weight: 2050 lb 929kg)

Power plant: 1× Lycoming O-435-1, 185hp kW)

Per for mance

Never exceed speed: 145 knots 163 mph)

Stall speed: 38 knots 42 mph, km/h)

Range: 375 nm no reserve )

Service ceiling: 15,800 ft 4,815.60m)

Rate of climb: ft/min m/s)



Wing loading: lb/ft² kg/m²)

Power/mass: hp/lb W/kg)

Ar mament

none

especificaciones aviones chuck yeager

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