The effort was confined primarily to a review of the existing Lockheed reports, assembly of available physical properties of the propellants and initiating a simplified analysis to give the order of magnitude values as an aid to specifying the important sources of forces resulting from heat transfer. (Author)
Study of Forces on Propellants Due to Heat Transfer Influencing Propellant Temperature in a Recovery Type Vehicle
1962
2 pages
Report
Keine Angabe
Englisch
REENTRY VEHICLES , ROCKET PROPELLANTS , HEAT TRANSFER , PROPELLANT TANKS , TEMPERATURE , REVIEWS , NITRIC ACID , HELIUM , DIMETHYL HYDRAZINE (1-1) , NITROGEN COMPOUNDS , DIOXIDES , THERMAL CONDUCTIVITY , SPECIFIC HEAT , VISCOSITY , DIFFUSION , WEIGHTLESSNESS , TEST EQUIPMENT , AGENA , NITROGEN OXIDES
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