Limit load factor: n=8
Ultimate load factor: n=12
IAS limit: V=1,150 km/h
Mach limit (flutter): M=1.03
Dynamic pressure limit: 6,400 kg/m²
Limit load factor: n=8
Ultimate load factor: n=12
IAS limit: V=1,150 km/h
Mach limit (flutter): M=1.03
Dynamic pressure limit: 6,400 kg/m²
youtu.be/9pV5_B2psPM
Several landing attempts seems to have been done with only one afterburning nozzle, perhaps simulating an engine-out scenario?
youtu.be/9pV5_B2psPM
Several landing attempts seems to have been done with only one afterburning nozzle, perhaps simulating an engine-out scenario?
It's the newest game from the rebirthed Microprose, who made all my favourite games when I was a sprog (and has a mission that's a reimplementation of the game Better Part of […]
[Original post on mastodon.rhys.wtf]
It's the newest game from the rebirthed Microprose, who made all my favourite games when I was a sprog (and has a mission that's a reimplementation of the game Better Part of […]
[Original post on mastodon.rhys.wtf]
6: Drive pile. Variable geometry Plutonium flanges.
7: Bussard sorter. Refines accumulated reactive elements into afterburning fuel.
8: Radshield. Baseplate of engineering section.
9: Turbopumps. Reaction mass injected at high pressure.
6: Drive pile. Variable geometry Plutonium flanges.
7: Bussard sorter. Refines accumulated reactive elements into afterburning fuel.
8: Radshield. Baseplate of engineering section.
9: Turbopumps. Reaction mass injected at high pressure.
flightopportunities.ndc.nasa.gov//media/uploa...
flightopportunities.ndc.nasa.gov//media/uploa...
The F110-GE-129 afterburning turbofan will be equipped with the Axisymmetric Vectoring Exhaust Nozzle to provide thrust vectoring during VTOL operations and flight.
Story: theaviationist.com/2025/11/07/s...
The F110-GE-129 afterburning turbofan will be equipped with the Axisymmetric Vectoring Exhaust Nozzle to provide thrust vectoring during VTOL operations and flight.
Story: theaviationist.com/2025/11/07/s...
Makes me believe Operation Spiderweb was a little more impactful than they let on.
Tu-160 is supersonic, so the maintenance burden is much higher (vibration, heat stresses, etc), and the engines (afterburning turbofan) need much more frequent overhauls.
Russia has rarely used the Tu-160 because of its importance to the nuclear triad.
Makes me believe Operation Spiderweb was a little more impactful than they let on.
Tu-160 is supersonic, so the maintenance burden is much higher (vibration, heat stresses, etc), and the engines (afterburning turbofan) need much more frequent overhauls.
➰ With its newly integrated afterburning engine, KIZILELMA is expected to near supersonic speeds while maintaining superior maneuverabilit
➰ With its newly integrated afterburning engine, KIZILELMA is expected to near supersonic speeds while maintaining superior maneuverabilit
It's a Vauxhall Omega Hearse with a afterburning Rolls Royce Viper turbojet where the stiffs should go.
It's a Vauxhall Omega Hearse with a afterburning Rolls Royce Viper turbojet where the stiffs should go.
38,000 afterburning lbs of thrust (each) at takeoff, 43% thermodynamic efficiency at cruise. In the 1970s. 🤯
Via the Heritage Concorde FB group.
38,000 afterburning lbs of thrust (each) at takeoff, 43% thermodynamic efficiency at cruise. In the 1970s. 🤯
Via the Heritage Concorde FB group.