SpaceX's Falcon Launches... Sort Of

JHarrison writes "Spaceflight Now is running a story on the SpaceX Falcon 1 launch yesterday. Those of you watching the stream will have no doubt noticed the telemetry failure at 04:50, and turns out that was more than them turning the webcast off.. "A year after its maiden flight met a disastrous end, the SpaceX booster lifted off at 9:10 p.m. EDT (0110 GMT Wednesday) from a remote launch pad on Omelek Island, part of a U.S. Army base at Kwajalein Atoll in the Marshall Islands. Controllers lost contact with the Falcon during the burn of the second stage that would have placed the rocket into orbit around Earth. "We did encounter, late in the second stage burn, a roll-control anomaly," Elon Musk, founder and chief executive officer of Space Exploration Technologies Corp., said in a post-launch call with reporters. Live video from cameras mounted aboard the rocket's second stage showed increasing oscillations about five minutes after liftoff, just before the public webcast was cut off. The rolling prevented the necessary speed to achieve a safe orbit, instead sending the stage on a suborbital trajectory back into the atmosphere.""

Comments

Engine bump and second stage control

[decaym]

Did anyone else notice the bump the Kestrel engine took during stage separation? On the 40MB video from SpaceX, it happend at 3:28 in or at T+00:02:52 on the screen clock. Maybe this is normal for the engine, but it was rather odd looking to me.

Also, there was a story earlier that the 2nd launch was delayed "due to concerns over a thrust vector control pitch actuator on the Falcon 1 booster's second stage". I wonder if this came back to bite them?

Finally, I'm impressed as hell that they could experience an abort after engine start yet still cycle back and launch in just another hour! When the Shuttle once aborted after engine start it took them a month to change out the engines and try again.

Re:Insightful...?

[ePhil_One]

Haven't we been sending rockets up into space for quite some time now. I'd think the fundementals should be down pretty pat now, the time for spectacular failures has past.

And yet we've lost two Space shuttles in recent memory. Space is not easy, rockets are enormously powerful devices that require light weight and experience a vast array of environments. Here a relatively minor thing went wrong, too much rotation, and the whole thing is now gone. Knowing how to do something and actually doing it are radically different things...

Re:That's how it works

[Keebler71]

Did anyone else watching the video notice the apparent contact between the 2nd stage nozzle and the interstage? I wonder if a TVC actuator was damaged leading to the nutation...

Re:That's how it works

[khallow]

Or it means that he's out of money for more test launches. He has demonstrated two difficult aspects, liftoff and stage seperation. So I'm optimistic. But as I recall, he's said in the past that he'll evaluate the program after the first three launches. So far, he's had one utter failure and one that lost control in the second stage. He still needs to put something in orbit.

Re:Rocket Science?

[Rei]

It's not really the fact that it's not from one of the bloated aerospace giants that makes this cheap (although I'm sure it doesn't hurt). It's also not true that they're not doing something that hasn't been done before. For example, I'm having trouble thinking of any rockets that use their particular mix of pressure and structural stabilization. For example, some Atlas stages use "balloon tanks" that will outright collapse under their weight if not kept pressurized. Most other rockets are structurally stable that, were it not for the lack of propellants, they could launch without being pressurized and remain intact. Pressurization is just added support. The Falcon concept is a hybrid of this: it has enough support that it can be transported and erected unpressurized... barely. This makes transport and handling costs cheaper and less error prone than for balloon tank-based rockets, but gives a higher payload fraction than rockets which have better structural support.

It's not without it's risks, of course. For example, it made the Falcon vulnerable to an accident a while back on Kwaj in which a reduction of pressure when draining a tank caused the tank to buckle. But in general, I think it makes for a nice design.

Falcon really is, for the most part, a "from scratch" rocket, so there's a lot of new ground covered. Not everything is from scratch, of course; I seem to recall, as an example, that their pintle injectors for the Merlin were pretty much borrowed as-is from Apollo. They're also not having to do much materials science, although they helping pioneering some fields (for example, friction-stir welding; a few older rockets have switched to using it as well, but it's still pretty new to rocketry).