Search filter

    • Year
      1906
      2018
    • Length
      9 m
      15 m
    • Height
      3 m
      5 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      17 m2
      27 m2
    • Wingspan (Beam)
      10 m
      16 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      26
    • Disc area
      1 m2
      460 m2
    • Main rotor diameter
      1 m
      62 m
    • Rotor number
      1 qt
      8 qt
    • Blades per rotor
      4 qt
      5 qt
    • Disc loading
      17 kg/m2
      73 kg/m2
    • Tail rotor diameter
      0 m
      5 m
    • Empty weight
      4341 kg
      6513 kg
    • Max. takeoff weight (Gross weight)
      6108 kg
      9164 kg
    • Loaded weight
      5 kg
      242500 kg
    • Crew
      1 per.
      3 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      96 km/h
      1500 km/h
    • Max. Speed
      746 km/h
      1120 km/h
    • Сruise Speed
      568 km/h
      852 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      107 km/h
      1050 km/h
    • Fuel Capacity
      23 l
      320000 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      0 hp
      60000 hp
    • Thrust
      21 kN
      33 kN
    • Service ceiling
      9753 m
      14631 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      1248 km
      1874 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      2 h
      4 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      1543 m/min
      2316 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      1 qt
      18 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      120 qt
      180 qt
    • Price
      41 USD
      750000000 USD

Lockheed T-1 Seastar

TypeAircraft
Company

Lockheed Corporation

Scheme

Low wing

Monoplane

Geometry
Length (m)
1.9
 
11.8
88.7
Height (m)
0.6
 
4.1
50.1
Wings
Wing area (m2)
1.1
 
22.3
925
Wingspan (Beam) (m)
0.1
 
13.1
95
Weights
Empty weight (kg)
8
 
5,427.2
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,636
575,000
Capacity
Crew (per.)
1
 
2
112
student and instructor
Speeds
Max. Speed (km/h)
25
 
933
28,165
at 10670 m
Сruise Speed (km/h)
52
 
710
3,087
Power
Thrust (kN)
1.5
 
27.2
1,914
1 powerplant
Performance
Service ceiling (m)
0.6
 
12,192
161,544
Range (Ferry range) (km)
4
 
1,561.2
40,700
Endurance (h)
0.0
 
3.1
150
Dynamic Performance
Rate of climb (m/min)
1.9
 
1,929.4
36,000
Stat
Number built (qt)
0
 
150
43,000
Introduction 1955
First flight 15.12.1953
Stop production 1970

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