Difference between revisions of "DAS-20 Gargantua"
m |
m (→Characteristics) |
||
Line 95: | Line 95: | ||
'''Type:''' Strike aircraft<br> | '''Type:''' Strike aircraft<br> | ||
'''Dimensions'''<br> | '''Dimensions'''<br> | ||
− | Wings: Type: variable geometry (aft-sweep); span: 49.58 m (unswept), 25.76 m (fully swept); wing area: 218.94 m | + | Wings: Type: variable geometry (aft-sweep); span: 49.58 m (unswept), 25.76 m (fully swept); wing area: 218.94 m<small><sup>2</sup></small>; aspect ratio: 11.23<br> |
Fuselage: Length: 54.61 m; height: 8.27 m<br> | Fuselage: Length: 54.61 m; height: 8.27 m<br> | ||
Weights: Airframe only: 106,150 kg; with engines: 120,255 kg; clean: 212,719 kg; operational: 228,181.6 kg; maximum take-off: 230,000 kg<br> | Weights: Airframe only: 106,150 kg; with engines: 120,255 kg; clean: 212,719 kg; operational: 228,181.6 kg; maximum take-off: 230,000 kg<br> | ||
'''Engines'''<br> | '''Engines'''<br> | ||
− | Type: 4 | + | Type: 4 × Lethe Aero-engines Corporation (LAC) ATG-25F2 hybrid turbofan/pulse detonation engines with two-dimensional thrust vectoring (deflagration phases only)<br> |
Dimensions: Outer diameter: 1.36 m; length: 7.13 m<br> | Dimensions: Outer diameter: 1.36 m; length: 7.13 m<br> | ||
Bypass ratio: 0.78<br> | Bypass ratio: 0.78<br> | ||
Weight: 3526.45 kg each<br> | Weight: 3526.45 kg each<br> | ||
− | Thrust (static): Military (deflagration): | + | Thrust (static): Military (deflagration): 13500 kgf; detonation: 25000 kgf<br> |
'''Fuel'''<br> | '''Fuel'''<br> | ||
Capacity: 114,200 litres<br> | Capacity: 114,200 litres<br> | ||
− | Weight (JP5): | + | Weight (JP5): 91360 kg<br> |
Fuel fraction: 0.42<br> | Fuel fraction: 0.42<br> | ||
− | '''Payload:''' | + | '''Payload:''' 16000 kg<br> |
'''Bays/Hardpoints/Stations'''<br> | '''Bays/Hardpoints/Stations'''<br> | ||
− | Main weapons bay ( | + | Main weapons bay (12000 kg - usually two GWS.58A Hurricane air-to-surface missiles)<br> |
− | 4 | + | 4 × smaller bays (1000 kg each - usually one GWS.84A Peregrine and one [[GDS.95 Firefly]])<br> |
'''Performance (Projected)'''<br> | '''Performance (Projected)'''<br> | ||
Speed (maximum): tba<br> | Speed (maximum): tba<br> |
Revision as of 07:09, 20 January 2007
Profile (n/a) | |
DAS-20 Gargantua | |
---|---|
Design details | |
Type | Strike aircraft |
Manufacturer | Detmerian Aerospace |
Design No. | DAS-20 |
Unit cost | B.1: $1768.35 million |
Service dates | 2005-present |
General characteristics | |
Crew | 4 |
Length | 54.61 m |
Wingspan | 25.76 m (swept)–49.58 m (unswept) |
Height | 8.27 m |
Empty weight | 120255 kg |
Payload | 16000 kg |
MTOW | 230000 kg |
Flight characteristics | |
Engines | 4 × LAC ATG-25F2 |
Speed | Mach 3+ |
Manoeuvrability | g |
Thrust loadings | Military: (cl.)–(max.) Reheat: (cl.)–(max.) Detonation: (cl.)–(max.) |
Fuel fraction | 0.42 |
Range | km |
Ceiling | 33000+ m |
Rate of climb | |
Armament | |
Internal | See Characteristics |
External | See Characteristics |
Operators | |
Unknown |
The DAS-20 Gargantua is an experimental high speed, high altitude heavy strike aircraft powered by hybrid turbofan-pulse detonation engines designed by Detmerian Aerospace Dynamics. It is unknown whether any production models of these aircraft ever entered operational service.
Characteristics
Crew: 4; pilot, co-pilot, and offensive and defensive measures operators (OMO and DMO)
Type: Strike aircraft
Dimensions
Wings: Type: variable geometry (aft-sweep); span: 49.58 m (unswept), 25.76 m (fully swept); wing area: 218.94 m2; aspect ratio: 11.23
Fuselage: Length: 54.61 m; height: 8.27 m
Weights: Airframe only: 106,150 kg; with engines: 120,255 kg; clean: 212,719 kg; operational: 228,181.6 kg; maximum take-off: 230,000 kg
Engines
Type: 4 × Lethe Aero-engines Corporation (LAC) ATG-25F2 hybrid turbofan/pulse detonation engines with two-dimensional thrust vectoring (deflagration phases only)
Dimensions: Outer diameter: 1.36 m; length: 7.13 m
Bypass ratio: 0.78
Weight: 3526.45 kg each
Thrust (static): Military (deflagration): 13500 kgf; detonation: 25000 kgf
Fuel
Capacity: 114,200 litres
Weight (JP5): 91360 kg
Fuel fraction: 0.42
Payload: 16000 kg
Bays/Hardpoints/Stations
Main weapons bay (12000 kg - usually two GWS.58A Hurricane air-to-surface missiles)
4 × smaller bays (1000 kg each - usually one GWS.84A Peregrine and one GDS.95 Firefly)
Performance (Projected)
Speed (maximum): tba
Cost
Airframe: $ 1698.27 million (with electronics, without engines)
Engines: $17.52 million each
Unit: $ 1768.35 million
Topics on Isselmere-Nieland | ||
---|---|---|
Category | Factbook Categories: Administrative divisions | Constitution | Defence Forces | Festivities | Government | Languages | Laws |