defaultluser
[H]F Junkie
- Joined
- Jan 14, 2006
- Messages
- 14,398
I did. Perhaps you should do it as well. You'd see that you explained the advantage of landing downrange from the launch location which I don't dispute for a second. What you didn't explain was the advantage of an ocean landing vs picking a remote spot on land. If your craft is in orbit already then you could simply hold the orbit a bit longer to reach your target re-entry point. I'd be surprised if they aren't already doing this now since a slow moving barge isn't going to be able to reposition itself much to catch up to a rocket moving at many time the speed of sound to account for some uncontrolled variable. You'd make the correction with the rocket in flight.
The advantages of a land target:
Doesn't move
Doesn't rock
Doesn't need to be (re)positioned
Doesn't need to have all facilities packed into a self contained barge
Doesn't rely on relatively calm seas
Doesn't need to be able to transport an inherently unstable vertically positioned rocket
Doesn't require retrieval from the bottom of the ocean should something go wrong.
The advantages of a water target:
Cool youtube videos?
I'm asking a legitimate question about the mechanics of the launch, not questioning the amazing technical achievement that has been accomplished. There is no need to interpret it as an attack on someone's personal savior or fanboy favorite.
Then go read up on Delta-V budget:
Delta-v budget - Wikipedia, the free encyclopedia
The delta-v requirements for sub-orbital spaceflight are much lower than for orbital spaceflight. For the Ansari X Prize altitude of 100 km, Space Ship One required a delta-v of roughly 1.4 km/s. To reach low Earth orbit of the space station of 300 km, the delta-v is over six times higher about 9.4 km/s. Because of the exponential nature of the rocket equation the orbital rocket needs to be considerably bigger.
The higher the orbit, or the LARGER the satellite, the higher the delta-V budget is.
Delta v = fuel consumption. END OF STORY.
KEY TO NOTE HERE: THE PAYLOAD SIZE AND ORBIT DETERMINE HOW MUCH FUEL YOU HAVE REMAINING DURING LANDING. Space X can't just ask the guys nicely if they'd like to reduce the orbit altitude, or if they could maybe please cut the weight of the satellite in half; they have to work with whatever they have remaining in the tank.
This means sometimes they won't be able to land at all due to having too little thrust left (they don't have parachutes, so you have to use fuel to halt the falling rocket from terminal velocity down to ZERO).
SpaceX landing attempt failed, as expected | EarthSky.org
But most of the time they should have enough fuel left to land over water, and on the more rare occasion they have enough fuel left to return to land THEY WILL DO SO.
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