PROBLEM: The picture's occupant lies reclined — and that is exactly how Orion flies its crew: lying on their backs with knees bent at 90 degrees, held by a 5-point harness, concave headrest and shoulder and hip bolsters, with a crew impact attenuation system that slides the seat up to six inches on rails to absorb landing loads. NASA's crashworthy-seat research adds a parabolic seat pan that fits the occupant's body nearly conformally. But an attenuation system that has never been logged against a real landing load is a design claim, not a safety record.
SOLUTION: A reclined seat impact attenuation record: every seat logged with its attenuation travel, its load history, and its post-landing inspection result — so a reclined crew seat's protection is proven by its record, not by its shape.
EVIDENCE BASIS: DOCUMENTED — Orion crew seats (NASA): four seats, 1st to 99th percentile of body size (4 ft 10 in, 94 lb to 6 ft 5 in, 243 lb); launch/re-entry position lying on backs, knees bent 90°, feet on foot pans; 5-point harness, concave headrest, shoulder and hip bolsters, foot-pan peg locking into crew boots; crew impact attenuation system slides the seat up to six inches on rails. NASA crashworthy-seat study (NTRS 20090020569): recumbent quasi-fetal posture, parabolic hip-support path and seat pan. Sources: NASA "Crew Systems"; NASA NTRS.
| Idea priority | Low |
| Needed By | Not sure -- Just thought it was cool |
By clicking the "Post Comment" or "Submit Idea" button, you are agreeing to the IBM Ideas Portal Terms of Use.
Do not place IBM confidential, company confidential, or personal information into any field.