"Congrats to Jeff Bezos and the BO team for achieving VTOL on their booster
It is, however, important to clear up the difference between "space" and "orbit", as described well by https://what-if.xkcd.com/58/
Getting to space needs ~Mach 3, but GTO orbit requires ~Mach 30. The energy needed is the square, i.e. 9 units for space and 900 for orbit."
I feel still a bit unclear on this though: hasn't SpaceX been trying to land just the first stage module (which presumably doesn't try to achieve that Mach 30)? If so, what is the main difference -- just the size of the payload, or is the 1st stage of SpaceX itself already going a lot faster than the BO rocket? (or perhaps both).
This flight confirms they have achieved that goal, correct?
Is the extra fuel needed to make such a landing a big part of going to orbit? No.
The extra weight a enerby needed to land vertically has nothing to do with a 900 factor. Musk's tweet is thus equally disengenuous. It makes it sound like vertical landing a booster for a rocket going to orbit is tremendously harder than what BO did. It is not, it's the same ball park.
Orbital velocity is in the vicinity of 7500 to 8000 m/s. At that speed your KE is 1/2.m.v^2 which is about 32e6 Joules/kg.
Orbits are, conveniently, at about 320 km, so your PE is m.g.h, or about about 3.2e6 Joules/kg.
In other words, the energy to get to orbit is ten times the energy to get to the altitude of orbit, and this exercise only got to 1/3 of that. So the energy involved was about 1/30 of that required to put something in orbit.
It's still a fantastic achievement, and an important - nay, critical - step on the way to properly reusable rockets, but it does lend some perspective to it.
Blue Origin did a soft landing from above the Karman line. SpaceX is trying to do that from orbit. The former involves speeds 10x less and energies 100x less than the latter.
Still a hard thing to do no matter how you look at it, but the two goals are not trivial to compare.
The best numbers I can find say that the Falcon 9 stage separation is at around 80km and 2km/sec (2.8 MJ/kg of total energy), and the Falcon 9 has so far failed to land under power.
But what I see on video is Bezos landing a rocket and Musk blowing up a rocket.
I understand the technical differences, but in terms of media, this is a pure win.
The Falcon 9 first stage, if I recall correctly, is incapable of either hovering or slowly decending. The engine has simply too much power. A Falcon 9 first stage, stopped mid air has two choices, keep the motor on and go up, or turn the motor off and fall - and I don't think the motor has too many extra restarts available.
Because of this inability to hover the Falcon 9 first stage, SpaceX is attempting to have the rocket's vertical velocity reach zero at the exact moment the rocket reaches the pad. This is why when you watch the grasshopper or other SpaceX landing videos, you always wonder for a split second if the rocket has just smashed into the ground. In order for this to work, all nine axis (three each of position, rotation, and velocity) must be brought to zero at exactly the same fixed time. This is insane level control theory here.
Now this type of landing is theoretically possible - and I think it has been tested on the grasshopper at lower speeds, but it scares the willies out of me. There's almost no room for error nor for the chaos of the universe.
New Shepard on the other hand, comes to a hover about 100? feet above the pad, moves horizontally to be above the pad, stops, then lowers itself down. This is tremendously simpler since the rocket only really cares about one or two set of axis at a time, it does not have to be nearly as precise, and you have time to fix anything that's not lined up.
I'm still curious to see if SpaceX can pull off their landing style, or will instead change so that their first stages will be able to hover.
The important difference between this New Shepherd flight and those Falcon 9 tests is that the Falcon 9s launched payload to orbit. They burned all their fuel, leaving them with the incredibly difficult slam-landing manoeuver to manage at the end. They have gone close, very close, but have not yet got things entirely right.
So, although this was an impressive technological demonstration, it's a long way from demonstrating a relaunch capability. I look forward to seeing new developments.
It would seem that SpaceX remains in a totally different league. By only going vertical, this is a very limited "spacecraft", more akin to the Virgin spaceplane than SpaceX's launch vehicles. For proper access to space, rather than tourist hops, everyone wants to see a reusable launch vehicle --> a craft to actually boost something towards orbit rather than an altitude record. That means returning to some sort of landing after huge downrange progress. So while this is an impressive achievement for space tourism (roller-coasters for billionaires) I still see SpaceX's efforts as the more revolutionary.
To jump in with the inevitable SpaceX comparison. Worth noting is you see the Blue Origin booster: fall, slow, hover, correct any drift, descend then land. The SpaceX booster cannot hover, it has more thrust than it weighs.
The landing footage begins at 1:40.
Larry Ellison; Oracle: http://www.superyachtfan.com/larry_ellison.html (including his Americas Cup yachts)
James (Jim) Clark; Silicon Graphics, Netscape: http://www.superyachtfan.com/sailing_yacht_athena.html
Paul Allen; Microsoft: http://www.superyachtfan.com/paul_allen.html (3 very large vessels)
And more recently:
Larry Page; Google: http://www.superyachttimes.com/yachts/details/333
Now you need a rocket! OK, Paul Allen did go there first, as far as I can tell.
https://www.reddit.com/r/spacex/comments/3u2gwm/apparently_b...
Is this gonna turn into a price war ?
As the great philosopher Mike Tyson once said: I'm a dreamer. I have to dream and reach for the stars, and if I miss a star then I grab a handful of clouds.
https://www.youtube.com/watch?v=9ZDkItO-0a4
The New Shepard went much higher though (100.5km vs 744m).