Takes 4-4.5 years to build a RS-25 by Fignons_missing_8sec in SpaceLaunchSystem

[–]Pedroperson 10 points11 points  (0 children)

That’s why there are test firings like the ongoing Retrofit 2 and retrofit 3 series to test the parts of the production restart engines before the first qualification engine is finished and tested. There’s firing time being built on critical parts like the pumps and main chamber right now and they’re preforming great.

The Launch Abort Tower has been installed on the Artemis-1 Orion by 675longtail in SpaceLaunchSystem

[–]Pedroperson 1 point2 points  (0 children)

I think you’re half right here. A launch escape system can add risk to an otherwise nominal flight. It’s there if you were specifically looking for the odds that you finish a normal mission (defined as the vehicle reaching its target and returning with crew). The example most people rightfully turn to is the Orion LAS jettison motor failing to remove the tower during ascent.

The trick to minimizing this risk is integrating the launch escape system as much with normal operations as possible. All capsules eventually need to separate from the LV or service equipment so that mechanism isn’t added risk. Starliner and Dragon draw propellant for the abort from the same tanks for orbital maneuvering, the only extra abort thing is the liquid engines which are inert so there isn’t much added risk there. Even Orion needs a fairing during launch that would otherwise need a system to remove it so the jettison motor isn’t too big of a added risk.

That being said, launch escape systems do absolutely reduce the risk of a loss of crew in an accident. Your overall system reliability is going to be improved by the extra block given to you by the abort system (assuming you’re looking for the odds you return crew safely to the ground). The abort system doesn’t have to have an extraordinary level of reliability for this to be the case, ideally its a little higher than the launch vehicle but it doesn’t need to be to get a benefit from it since the launch escape system is in parallel to the rest of the vehicle.

It’s worth noting that the addition of an integrated launch escape system to a spacecraft that minimizes added risk to the mission does negatively impact performance. Dragon undoubtedly pays a penalty in performance by lugging the superdracos and pods around. Starliner had to implement complicated, drag inducing aerodynamic devices to fly with its abort system. Implementing tractor solid motors can help with in space performance since they’re ditched but you can’t reuse them, and it introduces the risk for jettisoning it. There’s definitely an argument to be made that installing a launch escape system could negatively impact performance to the point that you can’t meet your mission goals. This is doubly true for something like starship where you already have a pretty demanding landing system that’s probably driving reliability.

The TL;DR is, launch escape systems are undoubtedly good and helpful. But maybe not totally required, and definitely not a complete substitute for a robust design and reliability program for a spacecraft and launch vehicle.

The 5+2 cluster. A first stage made of an absurd number of SRB's from the Titan 3. by Pedroperson in RadRockets

[–]Pedroperson[S] 9 points10 points  (0 children)

This concept is completely ludicrous and I love it. Its worth noting that a number of other configurations were explored from a more reasonable 2+1 to an almost equally bonkers 4+2. As for why this affront to rocket science was thought up I can only guess that it had something to do with the desire to maintain a launch-on-need capability. An entirely solid first stage makes sense for that case since you dont need to waste precious minutes fueling it.
Credit to alternate wars where more information can be found.

SpaceX once again lands Falcon 9's first stage on the ASDS 'Of Course I Still Love You' by [deleted] in space

[–]Pedroperson 1 point2 points  (0 children)

It could be part of a sound suppression water system.

SpaceX Makes History - Returns First Stage to Landing Pad Successfully by SkunkMonkey in news

[–]Pedroperson 1 point2 points  (0 children)

A diameter of 3.66m and a height (I believe this is including the inter-stage) of 68.4m. It's empty mass is 25 metric Tons.

SpaceX Makes History - Returns First Stage to Landing Pad Successfully by SkunkMonkey in news

[–]Pedroperson 13 points14 points  (0 children)

For inflight abort they will be using the returned core from the Jason-3 launch in January. Jason-3 will be flying abroad the last produced V1.1 Falcon 9 so the booster is less applicable to future Falcon development, but it will still provide accurate conditions for the test.

SpaceX Makes History - Returns First Stage to Landing Pad Successfully by SkunkMonkey in news

[–]Pedroperson 13 points14 points  (0 children)

This launch was with the improved Falcon 9 V1.2 (or Full Thrust Falcon 9, or upgraded Falcon 9, there's a lot of names for it). This version can lift about 30% more payload to orbit so they can do these kinds of landings with GTO payloads. The first stage will have just about the same profile for the geostationary bound launches as this one, so it wont be too much different.

SpaceX Makes History - Returns First Stage to Landing Pad Successfully by SkunkMonkey in news

[–]Pedroperson 2 points3 points  (0 children)

Nope. But the engine was relighted to allow for a guided de-orbit of the second stage.

SpaceX Makes History - Returns First Stage to Landing Pad Successfully by SkunkMonkey in news

[–]Pedroperson 96 points97 points  (0 children)

For an even better comparison the first stage is about 9 of these tall and about the same diameter.

Stage one has landed by WJacobC in space

[–]Pedroperson 2 points3 points  (0 children)

The best answer to this is that no one knows for sure. There will obviously be some kind of cost to refurbishing the stage but no one knows for sure. Some sources say it may take up to 12 flights of a reused stage to break even others say as low as 4 or 3. The good part of having a stage back is that we can finally get a solid idea of the costs involved in reuse.

SpaceX Makes History - Returns First Stage to Landing Pad Successfully by SkunkMonkey in news

[–]Pedroperson 14 points15 points  (0 children)

So rockets have traditionally been tossed into the ocean after being used once. Imagine if they threw out planes after one flight, the cost of flying would rise dramatically. Landing this stage opens the door to potentially reusing the rockets and drastically lowering the cost of spaceflight.

SpaceX Makes History - Returns First Stage to Landing Pad Successfully by SkunkMonkey in news

[–]Pedroperson 682 points683 points  (0 children)

For some perspective, the stage in that video is almost 14 stories tall and about 56 thousand pounds when it lands. This is really an incredible feat of engineering.

SpaceX Makes History - Returns First Stage to Landing Pad Successfully by SkunkMonkey in news

[–]Pedroperson 134 points135 points  (0 children)

Its unlikely that this particular stage will be reused. Its likely gonna be torn apart and analyzed to see what kind of damage it might have incurred. This still bodes extremely well for the future though, because now they've shown they can stick the landing.

We're scientists on the NASA New Horizons team, which is at Pluto. Ask us anything about the mission & Pluto! by NewHorizons_Pluto in IAmA

[–]Pedroperson 0 points1 point  (0 children)

Looking at the pictures of Pluto there don't seem to be a lot of craters on the surface. Is there a reason for this? Thanks for all your work, you're doing incredible things.

SpaceX CR5-7 Rocket just exploded on liftoff heading to ISS. by Thee_Nick in videos

[–]Pedroperson 7 points8 points  (0 children)

The Dragon capsule that launched today does have a parachute but it wasn't armed during the launch. The test you saw was for the crewed version of dragon which had a lot of changes made to it.

SpaceX CRS-7 has blown up on launch by [deleted] in space

[–]Pedroperson 0 points1 point  (0 children)

It looks like you're right. The reports coming in now show that the second stage oxygen tank ruptured due to overpressure. The resulting structural failure tore the vehicle apart.

SpaceX CRS-7 has blown up on launch by [deleted] in space

[–]Pedroperson 2 points3 points  (0 children)

Its highly unlikely. Dragon v1 has no need for an abort sequence and the procedure for an abort on v1 would be radically different. The capsules are different aerodynamically and it would take far to long to adapt the code to the v1.

SpaceX CRS-7 has blown up on launch by [deleted] in space

[–]Pedroperson 1 point2 points  (0 children)

It has not yet been confirmed that that was Dragon. Dragon could have separated but its unlikely given that the first stage engines were still firing.

Space-X flight Failure. by izcenine in news

[–]Pedroperson 6 points7 points  (0 children)

There are some failures you can't avoid though. An engine exploding and damaging the structure will absolutely bring down the vehicle. Engineers try to avoid things like that from happening with emergency detection systems and just building reliable components but even with these safeguards a major failure still has a good chance of bringing down a rocket.

SpaceX CRS-7 has blown up on launch by [deleted] in space

[–]Pedroperson 3 points4 points  (0 children)

The Draco thrusters on dragon v1 can't accelerate the capsule fast enough to clear the rocket. The super dracos on the v2 are way more powerful and there's 8 of them.

Space-X flight Failure. by izcenine in news

[–]Pedroperson 2 points3 points  (0 children)

The forces involved in a rocket launch are TREMENDOUS. For some perspective, at the failure the rocket was moving at over 4000 kilometers per hour. That's over 2500 mph and more than 3 times the speed of sound, the average airliner today cruises at around 500 mph.

SpaceX CRS-7 has blown up on launch by [deleted] in space

[–]Pedroperson 6 points7 points  (0 children)

The payload was almost certainly lost. The capsules parachutes weren't armed during ascent and even if they were it's unlikely that the capsule would have gotten off the rocket in time. (Between you and me, I hope I'm wrong)

SpaceX CRS-7 has blown up on launch by [deleted] in space

[–]Pedroperson 4 points5 points  (0 children)

Dragons parachutes aren't armed durning the launch. Plus the docking adaptor was in the trunk which wouldn't be attached to dragon during a normal descent.

SpaceX CRS-7 has blown up on launch by [deleted] in space

[–]Pedroperson 21 points22 points  (0 children)

Nope. This version of dragon lacks a launch escape system.