Claim

0

The Upward Acceleration Target of 17.3 G's for 6.8 Seconds is Reasonable

rampupward accelerationg-force countermeasuresimmersion

Evidence

The upward-acceleration target applies to the ramp that redirects the vehicle skyward after horizontal acceleration. Allowing up to ~17 g (normal to the trajectory) over a short, controlled interval (≈6.8 s) enables a smaller minimum curvature radius and therefore a shorter ramp, expanding siting options without altering the upstream acceleration profile. In practice, the vehicle's speed and the ramp's radius of curvature generate 160 m/s2 of centrifugal acceleration in addition to the 9.8 m/s2 of acceleration due to Earth's gravity, for a total of 169.8 m/s or 17.3 g.

The upward-acceleration target is a design input for sizing the ramp curvature and associated structures; it propagates through engineering and economic models into the cost estimate of the launch system. For baseline economics, we assume operations across 10 Mars transfer windows with crews of highly trained, physically fit astronauts adapted to Earth gravity.

In +Gx (“eyes-in”) orientation, the load vector is aligned front-to-back through the torso, which markedly increases human tolerance relative to +Gz. The crew rides in water-immersion acceleration couches that rotate to maintain +Gx during the pitch-up. Historical human-tolerance data with water immersion show sustained tolerance of 12 g for exposures of up to ~4 minutes; for much shorter exposures (seconds rather than minutes), higher peaks should be tolerable with appropriate countermeasures. (A representative chart from “Human Tolerance to Some of the Accelerations Anticipated in Space Flight” is shown in the ISDC 2025 presentation: Electromagnetic Launch — What is (and is not) Holding it Back.)

In a 1960s study titled "A new method of protection against the effects of acceleration on the cardiovascular system", three male subjects were exposed to peak accelerations—limited to the maximum each felt comfortable enduring—of 26, 28, and 31 g. The acceleration followed a 25-second versine profile, and the subjects were protected inside a “total water immersion G-capsule.”

An example of a possible g-force countermeasure is a respiration protocol wherein, just prior to the onset of high acceleration, an assisted-breathing system helps to deflate the lungs to promote a more homogeneous density distribution within the thoracic cavity, then immediately reinflates them at the end of the high-acceleration period.

The end of the acceleration section and the beginning of the ramp will be engineered so that over a time period of one second, the load will shift from ~8 g forward to ~17.3 g upward, and the crew couches will rotate ~83° to maintain +Gx (eyes-in) orientation. The bed rotation follows a smooth ease-in/ease-out profile.

The claim is not that every crewmember can tolerate 17.3 G's indefinitely, but that with state-of-the-art countermeasures, the short (≈6.8 s) upward-acceleration window lies within a reasonable, testable envelope for an astronaut-rated system. Further validation testing and certification would refine the exact limit used for crewed operations.

Reviews

The following reviews are limited in scope to the validity of the claim made above, and do not imply that the reviewer has taken a position regarding any other claim or the overall feasibility of a concept that is supported by this claim.