The Price of the Bleeding Edge

Back in March I wrote about the history and reorganization of Artemis, focusing on the operational level of the program. Something I have routinely run into is conversations, comments, and questions about test failures in the industry. Recent publicly visible test failures from SpaceX and Blue Origin have brought up conversations about safety and waste from the programs and I wanted to bring some context to the matter. But to not bury the lede, Orbital-Vehicle development and operation has always and will continue to carry a standard of risk and complexity that is outside of what the public usually interfaces with. In Admiral Rickover’s famous 1953 Paper Reactor memo he touches on the reality with the following:

“Important decisions relative to the future development of atomic power must frequently be made by people who do not necessarily have an intimate knowledge of the technical aspects of reactors. These people are, nonetheless, interested in what a reactor plant will do, how much it will cost, how long it will take to build, and how long and how well it will operate. When they attempt to learn these things, they become aware of confusion existing in the reactor business. There appears to be unresolved conflict on almost every issue that arises.
I believe that this confusion stems from failure to distinguish between the academic and the practical. These apparent conflicts can usually be explained only when the various aspects of the issue are resolved into their academic and practical components.” [1]

This detachment of the operationalization of complex systems from their “paper” phase can create a strong reaction when things go wrong.

Figure 1: This is the engine cycle of the RS-25 engine used on the space shuttles. Here there are fluids at play, the H2 fuel and the O2 oxidizer. Both are pressurized by turbopumps driven by fuel rich preburners (the exhaust of the preburner powering the turbine is mostly unreacted H2). The H2 after being pressurized is flown through cooling channels throughout the engine. The O2 and H2 meet in the main injector and react in the main combustion chamber creating combustion products (mostly H2O) that are the propellant for the engine expelled through the nozzle to generate thrust.

Orbital-Vehicle systems are some of the most complex things humans have ever built and operated. To put things into perspective Figure 1 shows the high level engine cycle of the Space Shuttle Main Engine the RS-25. In it are 4 turbopumps, 2 preburners, a complex H2 regenerative cooling cycle, injector manifolds for the turbine preburners, and a main injector system. Each of these engine subcomponents represent large teams spending years of development work. And this is only one of 3 engines on the larger space shuttle of which if I were to dive into the subcomponents at even a high level this would be too long of a read. The point is Orbital-Vehicle systems are immensely complex systems playing at the edge of material science and dealing with extremely energy dense materials. A few or a single component failure can have catastrophic consequences. Figure 2[2] shows a histogram I compiled of Orbital-Vehicle development and operational failures from 1950 to the present. Of the 260 recorded, the bulk occurred during the period of 1957 to 1975. This correlates with the highest spending in space in US history with the most concurrent development programs. The recent failures you see on the news are not an historical and irresponsible aberration, they are the norm for this industry.

Figure 2: Year on Year breakdown of Orbital-Vehicle failures, anomalies, and explosions during their testing and operation from 1950 to 2026. Note the high cadence in the early Apollo era and the sharp reduction that has been maintained ever since. The spike starting in 2018 correlates with the beginning of Artemis and the spike in space spending and development. The period from the 1980s to the 2010s correlates to a period of low Orbital-Vehicle development before Artemis.

That tolerance for losing hardware is the deliberate flip side of a near-total intolerance for losing people. For all the failures in that dataset, fatalities are incredibly low for an industry carrying this much implicit risk. I compiled 29 Orbital-Vehicle-related fatalities from 1950 to 2026 (see Figure 3[2]). This dataset excludes weapons development and sub-orbital programs like the previous dataset. This number is so low because of the extreme care taken around human life in the space industry. Almost half of the fatalities are concentrated in the two space shuttle disasters and the most recent two in 2010 were in decommissioning solid rocket fuel. This tradition can really trace its roots to the Apollo 1 command module tragedy where astronauts Grissom, White, and Chaffee were tragically killed in a fire that broke out in a preflight test. Poor design of the capsule, particularly the inward-opening hatch, left the pad crew unable to reach them before they asphyxiated[3]. This led to a strong tradition of human safety that persists to this day.

Figure 3: Year on Year breakdown of Orbital-Vehicle related fatalities. The largest events were the two space shuttle disasters of Challenger and Columbia . Most recent was the 2 deaths in 2010 from an explosion working with solid rocket fuel.

Space really is the final frontier of human development. It offers a seemingly infinite series of bleeding edge problems to solve and overcome. The current objective of Lunar Permanence that the United States and other Space-Capable nations are targeting will require the continued development of these massively complex systems. There will be more accidents, but that's just part of the process of pushing to and beyond the limit.

Sources

  1. Paper Reactor, Admiral Hyman Rickover, 1953https://whatisnuclear.com/rickover.html
  2. Orbital Launch Faliures and Fatalities Dataset.https://github.com/jacobmills1997-sys/us-orbital-vehicle-failures/tree/main
  3. Apollo 1 Tragedy, National Air and Space Museum. https://airandspace.si.edu/explore/stories/apollo-missions/apollo-1

Meet the Author

Jacob Mills

Digital Ground Game

Jacob is a aerospace engineer currently working in industry specializing in fluids analysis. He also works with Digital Ground Game on their 2026 canvassing program for the midterm elections. Jacob enjoys spending as much time in his home mountain range,…

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