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It stands for Big Fucking Rocket.I ask Musk whether he really calls it that; his answer is both delightfully nerdy, and not.
I'm crossing my fingers for seeing BFR on the moon by the mid-2020s. 1.6k. This … My question(s) is regarding the first payloads on the cargo and human flights to Mars in the next 5-10 years.Will you be sending food and water rations for early colonists? The impact is so small. The SpaceX Starship is a fully-reusable launch vehicle and spacecraft that is being privately developed by SpaceX. The objective is to meet or exceed passenger airline levels of safety. Then consider the amount of material ADDED to Earth by meteoroids, etc.
It is quite small (and light) relative to the rest of the vehicle and is never actually used to generate lift in the way that an aircraft wing is used.It's true purpose is to "balance out" the ship, ensuring that it doesn't enter engines first from orbit (that would be really bad), and provide pitch and yaw control during reentry.When traveling to Mars they will have to be stored for months. Mission Profile. As excited as I am for upcoming Mars missions, I certainly believe that lunar missions will likely come first, whether as NASA missions or just SpaceX testing BFR's capabilities close to home.
They can also be molded to the necessary processes and tools, instead of having engrained routines and favored methods already. About a 1:4.5 ratio.For environmentally friendly earth to earth flights in the future they could switch to hydrolox propellant which has zero emissions, driving to to the port would be the most harmful part of the trip. * AstrobiologyPress J to jump to the feed. This board is not an official outlet for SpaceX information.Looks like you're using new Reddit on an old browser. Accurate nozzle profile obtained through pixel by pixel analysis of this photo [2] and these thermodynamic profiles are generated by isentropic flow equations.I will happily post the full research project when completed, so any assistance in verifying these results is greatly appreciated.If you find an event or conference for which a SpaceX representative will be in attendance, please message the moderators for inclusion in the sidebar!Welcome to r/SpaceX, the premier SpaceX discussion community and the largest fan-run board on the American aerospace company SpaceX. Press question mark to learn the rest of the keyboard shortcuts Heat transfer slowly but surely rises the temperature of the tanks, eventually boiling off the propellants.Will liquid methane and LOX have to be cooled - or is thermal insulation of the header tanks expected to be so good that no active cooling is required?If cooling is required, what kind of system will the BFS use to manage the temperature of propellants in zero-gee?The main tanks will be vented to vacuum, the outside of the ship is well insulated (primarily for reentry heating) and the nose of the ship will be pointed mostly towards the sun, so very little heat is expected to reach the header tanks. Launch is also around 1.3 T/W, so it will look pretty much like a launch in reverse....The sub-scale Raptor prototype has a (speculated) thrust of about ~100 tons-force currently, and will be scaled up to ~170 tons-force Can you tell us more about the current status and expected (best-case) timeline of this scale-up effort?Thrust scaling is the easy part. 18:01. Welcome to r/SpaceX, the premier SpaceX discussion community and the largest fan-run … Press J to jump to the feed. 214 comments. Everyday Astronaut 767,032 views.
It stands for Big Fucking Rocket.I ask Musk whether he really calls it that; his answer is both delightfully nerdy, and not.
I'm crossing my fingers for seeing BFR on the moon by the mid-2020s. 1.6k. This … My question(s) is regarding the first payloads on the cargo and human flights to Mars in the next 5-10 years.Will you be sending food and water rations for early colonists? The impact is so small. The SpaceX Starship is a fully-reusable launch vehicle and spacecraft that is being privately developed by SpaceX. The objective is to meet or exceed passenger airline levels of safety. Then consider the amount of material ADDED to Earth by meteoroids, etc.
It is quite small (and light) relative to the rest of the vehicle and is never actually used to generate lift in the way that an aircraft wing is used.It's true purpose is to "balance out" the ship, ensuring that it doesn't enter engines first from orbit (that would be really bad), and provide pitch and yaw control during reentry.When traveling to Mars they will have to be stored for months. Mission Profile. As excited as I am for upcoming Mars missions, I certainly believe that lunar missions will likely come first, whether as NASA missions or just SpaceX testing BFR's capabilities close to home.
They can also be molded to the necessary processes and tools, instead of having engrained routines and favored methods already. About a 1:4.5 ratio.For environmentally friendly earth to earth flights in the future they could switch to hydrolox propellant which has zero emissions, driving to to the port would be the most harmful part of the trip. * AstrobiologyPress J to jump to the feed. This board is not an official outlet for SpaceX information.Looks like you're using new Reddit on an old browser. Accurate nozzle profile obtained through pixel by pixel analysis of this photo [2] and these thermodynamic profiles are generated by isentropic flow equations.I will happily post the full research project when completed, so any assistance in verifying these results is greatly appreciated.If you find an event or conference for which a SpaceX representative will be in attendance, please message the moderators for inclusion in the sidebar!Welcome to r/SpaceX, the premier SpaceX discussion community and the largest fan-run board on the American aerospace company SpaceX. Press question mark to learn the rest of the keyboard shortcuts Heat transfer slowly but surely rises the temperature of the tanks, eventually boiling off the propellants.Will liquid methane and LOX have to be cooled - or is thermal insulation of the header tanks expected to be so good that no active cooling is required?If cooling is required, what kind of system will the BFS use to manage the temperature of propellants in zero-gee?The main tanks will be vented to vacuum, the outside of the ship is well insulated (primarily for reentry heating) and the nose of the ship will be pointed mostly towards the sun, so very little heat is expected to reach the header tanks. Launch is also around 1.3 T/W, so it will look pretty much like a launch in reverse....The sub-scale Raptor prototype has a (speculated) thrust of about ~100 tons-force currently, and will be scaled up to ~170 tons-force Can you tell us more about the current status and expected (best-case) timeline of this scale-up effort?Thrust scaling is the easy part. 18:01. Welcome to r/SpaceX, the premier SpaceX discussion community and the largest fan-run … Press J to jump to the feed. 214 comments. Everyday Astronaut 767,032 views.