EFFECT OF CONTACT ANGLE AND TANK GEOMETRY ON THE CONFIGURATION OF THE LIQUID-VAPOR INTERFACE DURING WEIGHTLESSNESS

R. C. Nussle, E. W. Otto, Daniel A. Petrash

NASA Technical Reports Server (NASA) · 1963 · 13 citations · 0 references

Concepts

Abstract

Effect of contact angle and space vehicle tank geometry on configuration of rocket propellant liquid-vapor interface during weightlessness