A “G” load suppressing aircraft incorporating a fuselage having a nose end; a cavity, extending downwardly into the fuselage, the cavity opening upwardly at the fuselage's nose end; a cockpit capsule fitted for receipt within the cavity; explosive bolts for releasably attaching the cockpit capsule to the fuselage, the explosive bolts holding the cockpit capsule within the cavity; a liquid supply line for filling the cockpit capsule with a transparent liquid, the liquid supply line being connected operatively to the cockpit capsule; and rocket engines for ejecting the cockpit capsule from the cavity, the rocket engines being connected operatively to the cockpit.
"G" Load Suppressing Aircraft
2024-09-26
Patent
Electronic Resource
English
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