For a Boeing B-52H, on a mission at maximum takeoff weight, what would
be the initial cruising altitude and true airspeed? How much fuel would
have been burned off in takeoff and climb?
My thanks in advance for all replies.
Peter Wezeman anti-social Darwinist
On Tue, 10 Aug 2021 15:27:56 -0700 (PDT), peterwezeman@hotmail.com wrote:
For a Boeing B-52H, on a mission at maximum takeoff weight, what would
be the initial cruising altitude and true airspeed? How much fuel would
have been burned off in takeoff and climb?
My thanks in advance for all replies.
Peter Wezeman anti-social Darwinist
OK - From the June 1969 B-52H Standard Aircraft Characteristics:'
Standard Day - 59 deg F/ 15 C, QNH 29.29" / 1003 mb
Max Takeoff Weight 488,000 lbs
Takeoff Ground RUn 7,420 ft (TO Power)
Takeoff Run to clear 50' 9,580 (TO Power)
Initial Cruising Alt: 31,950 ft
Average Cruise Sped (TAS) 453 Kts
Fuel Burn on the ground is about 150 lbs/minute
Fuel Burn for takeoff to climb sped is about 3,500 lbs
Fuel burn for climbout is about 12,500 lbs
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