История изменений
Исправление atsym, (текущая версия) :
- https://www.reddit.com/r/SpaceXLounge/comments/7z7vcr/summary_of_block_5_upgr...
- https://www.reddit.com/r/spacex/comments/80m1yd/first_falcon_9_block_5_booste...
- ☑ Titanium grid fins for unlimited re-uses.
- ☑ New landing legs with the ability to be retracted by the ground crew instead of having to be removed after landing. These legs will also be black instead of white.
- ☑ Changes to the turbopumps to prevent turbine wheel microfractures. This was never considered a risk by SpaceX but NASA asked SpaceX to fix the issue and from all reports they have.
- ☑ Replace paint with thermal protection barrier coating for the purposes of re-use.
- ☑ Improved heat shielding around the engines to improve re-usability.
- ☑ The octaweb (structure that holds the engines) will be bolted instead of welded, to reduce time for inspection/repair/refurbishment and to allow easy change from F9 to FH side booster.
- ☑ The interstage will be black instead of white - likely unpainted carbon fiber (saves time and weight).
- ☑ Upgraded fairing, Fairing 2.0, which is very slightly larger and has changes to allow for recovery and re-use. It is also easier to make and lighter than the previous fairings.
- ☑ SpaceX's upgraded COPVs (dubbed COPV 2.0) will fly on Block V. This is an upgrade to further reduce the potential for an incident like Amos-6.
- ☑ Another improvement in thrust for the Merlin 1D engines (roughly 10%).
- ☑ The rocket will be man-rated, meaning it will be certified to carry crew. NASA has set the bar at 7 successful flights of the rocket for certification.
- ☑ Upgrades to active components such as valves, as well as many other parts to allow for many re-uses.
- ☑ Improved flight control, angle-of-attack, and control authority which should allow for landings with less fuel (and therefore the ability to land after lofting heavier payloads).
Исправление atsym, :
- https://www.reddit.com/r/SpaceXLounge/comments/7z7vcr/summary_of_block_5_upgr...
- https://www.reddit.com/r/spacex/comments/80m1yd/first_falcon_9_block_5_booste...
- ☑ Titanium grid fins for unlimited re-uses.
- ☑ New landing legs with the ability to be retracted by the ground crew instead of having to be removed after landing. These legs will also be black instead of white.
- ☑ Changes to the turbopumps to prevent turbine wheel microfractures. This was never considered a risk by SpaceX but NASA asked SpaceX to fix the issue and from all reports they have.
- ☑ Replace paint with thermal protection barrier coating for the purposes of re-use.
- ☑ Improved heat shielding around the engines to improve re-usability.
- ☑ The octaweb (structure that holds the engines) will be bolted instead of welded, to reduce time for inspection/repair/refurbishment and to allow easy change from F9 to FH side booster.
- ☑ The interstage will be black instead of white - likely unpainted carbon fiber (saves time and weight).
- ☑ Upgraded fairing, Fairing 2.0, which is very slightly larger and has changes to allow for recovery and re-use. It is also easier to make and lighter than the previous fairings.
- ☑ SpaceX's upgraded COPVs (dubbed COPV 2.0) will fly on Block V. This is an upgrade to further reduce the potential for an incident like Amos-6.
- ☑ Another improvement in thrust for the Merlin 1D engines (roughly 10%).
- ☑ The rocket will be man-rated, meaning it will be certified to carry crew. NASA has set the bar at 7 successful flights of the rocket for certification.
- ☑ Upgrades to active components such as valves, as well as many other parts to allow for many re-uses.
- ☑ Improved flight control, angle-of-attack, and control authority which should allow for landings with less fuel (and therefore the ability to land after lofting heavier payloads).
Исходная версия atsym, :