TWO ROCKET INJECTORS USING WATER FLOW AND LIQUID NITROGEN FLOW
Summary
TWO ROCKET INJECTORS USING WATER FLOW AND LIQUID NITROGEN FLOW
NASA Identifier: C-1951-27691
Tags
nasa
two rocket injectors using water flow and liquid nitrogen flow
dvids
high resolution
glenn research center
aviation research organization
rocket engines
rocket technology
Date
1951
Location
Source
Defense Visual Information Distribution Service
Link
Copyright info
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