DTIC ADA042337: Crew Escape Capsule Retrorocket Concept. Volume I. Demonstration Program.Report as inadecuate



 DTIC ADA042337: Crew Escape Capsule Retrorocket Concept. Volume I. Demonstration Program.


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The retrorocket demonstration program was conducted to evaluate an alternative to the inflatable airbags that are currently used with crew escape capsules to attenuate the landing impact forces. In-house tests indicated that if the vertical impact velocity was ten feet per second or less, the impact forces would be within human tolerances. Analyses

Author: Defense Technical Information Center

Source: https://archive.org/



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