Copyright 2023 Robert Clark
I had earlier argued that SpaceX should withdraw the Starship as a lunar lander. The primary basis for this was for safety of the surrounding population in case of an explosion on launch, SpaceX should withdraw its application for the Starship as an Artemis lunar lander.
However, an additional reason why the Starship should not be used for a lunar lander is for safety of the crew. In the blog post, Did SpaceX throttle down the booster engines on the IFT-2 test launch to prevent engine failures?, I noted two separate methods of calculation suggest the SuperHeavy booster was throttled down to <75%. I also suggested the Starship upper stage was fired at ~90%. Given this difference in thrust power levels, I suggested the booster completed its portion of the ascent because it was throttled down and the upper stage did not because it was at close to full thrust.
Even though the booster engines successfully fired during the ascent, the booster exploded during the attempted return. One explanation offered was the engines were damaged by fuel slosh during flip of the booster. However, it should be noted the Starship during tests of the landing procedure, that at least one Raptor always leaked fuel and caught fire.
Since relighting the Raptors in flight always resulted in an engine fire, that is the most likely explanation for the IFT-2 booster explosion as well.
SpaceX Misleadingly Characterizes Raptor's Qualification for Flight.
SpaceX has been using the term "full duration" for their Raptor static fire tests when they might only last 5 seconds. In the rest of the industry other than SpaceX, a full duration static test means firing for the full duration of an actual launch.
For engines for a craft intended to carry astronauts and for which billions of dollars of public funds are earmarked there should be provided some indication about the safety and reliability of such engines. For instance this report provides estimates of the reliability of the different components of the SLS:
SLS-RPT-077
VERSION: 1
National Aeronautics and Space Administration
RELEASE DATE: MARCH 8, 2013
SPACE LAUNCH SYSTEM PROGRAM (SLSP)
RELIABILITY ALLOCATION REPORT
But no such estimates for the Raptor have been provided. That so many engines have consistently failed in actual flights suggest they have quite low reliability.
In the scenario of the Merlin engines used for crewed flight, over 80 missions of the Falcon 9 were successfully flown before the first crewed flight. That means over 800 successful firings of the Merlins during that time. And added on after that the many launches since then, over one thousand successful firings of the Merlins have been made.
Robert Clark
4 comments:
By your methodology the F-1 engines should never have been used...
This argument takes no account of the vulnerability of exposed plumbing and wiring in hot backwind conditions, or the differences between Raptor-1 and Raptor-2. A lot of the problems seen with the Starship-only flights would likely trace to pushing Raptor-1 too hard for thrust, and exposed plumbing and wiring failing in the hot gas exposures. -- GW
The F-1 engines were tested together at full thrust and full flight duration in static fires until they were proven to work:
Saturn V S IC Static Firing (archival film).
https://youtu.be/-rP6k18DVdg
Robert Clark
To Gary Johnson, in an upcoming blogpost I'll discuss that even the tests on the test stands suggest the Raptor is unreliable.
Robert Clark
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