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Bristol Brabazon vs Antonov An-225 Mriya (Cossack) Comparison


Aviation | Utilities | Side-by-Side Comparison

Direct side-by-side comparison of two aircraft.

Your selected aircraft are compared in side-by-side arrangement below. You can always go back and Compare any two aircraft in our database. Some entries contain '0', 'not available', or an 'NA' value. This is more common with conceptual, experimental, and x-plane designs. Rotary-wing system (i.e. helicopters) values include main rotor diameter as part of width/wingspan measurement. UAV entries may display crew values as '0', not taking into account ground-based controllers.
Subjects
Bristol Brabazon Mk.1
Commercial Airliner / Passenger Transport Aircraft
Antonov An-225 Mriya (Cossack)
Heavy-Lift Strategic Long-Range Transport Aircraft
Basics
ORIGIN
United Kingdom
ORIGIN
Soviet Union
YEAR
1949 [Diff.-40 yrs]
YEAR
1989 [Diff.+40 yrs]
CREW
6
CREW
6 or 7
PRODUCTION
1 units [Diff.0]
PRODUCTION
1 units [Diff.0]
Dimensions
LENGTH
177.2 ft (54.0 m) [Diff.-98.4 ft]
LENGTH
275.6 ft (84.0 m) [Diff.+98.4 ft]
WIDTH/SPAN
229.7 ft (70.0 m) [Diff.-60.4 ft]
WIDTH/SPAN
290.0 ft (88.4 m) [Diff.+60.4 ft]
HEIGHT
49.2 ft (15.0 m) [Diff.-10.5 ft]
HEIGHT
59.7 ft (18.2 m) [Diff.+10.5 ft]
Relative Size Comparison
Shapes below depict aircraft from wingtip-to-wingtip / nose-to-tail assuming aircraft are being viewed from overhead perspective (the nose pointing towards the top of the screen). Helicopter widths include main rotor diameter. If any dimensional values are "NA" in the database then the presented shapes may appear skewed.
Compare aircraft size graphic
Bristol Brabazon Mk.1
Compare aircraft size graphic
Antonov An-225 Mriya (Cossack)
Weights
EMPTY WT.
145,108 lb (65,820 kg) [Diff.-240,701 lb]
EMPTY WT.
385,809 lb (175,000 kg) [Diff.+240,701 lb]
M.T.O.W.
286,601 lb (130,000 kg) [Diff.-1,036,173 lb]
M.T.O.W.
1,322,774 lb (600,000 kg) [Diff.+1,036,173 lb]
Installed Power
8 x Bristol Centaurus radial piston engines developing 2,650 horsepower each.
6 x ZMKB Progress (Lotarev) D-18T turbofan engines developing 51,587 lb of standard thrust each.
Performance
SPEED
298 mph (480 kph) [Diff.-230 mph]
SPEED
528 mph (850 kph) [Diff.+230 mph]
RANGE
5,530 miles (8,900 km) [Diff.+2,734 miles]
RANGE
2,796 miles (4,500 km) [Diff.-2,734 miles]
CEILING
24,934 ft (7,600 m) [Diff.-11,155 feet]
CEILING
36,089 ft (11,000 m) [Diff.+11,155 feet]
Armament
None.
None.
Going Further
View Entry
(Bristol Brabazon)
View Entry
(Antonov An-225 Mriya (Cossack))
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