New approaches for fundamental rocket injector studies using a shock tube

Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference

Volumn 5, Issue , 2006, Pages 4035-4043

  Rotavera, Brandon ^a,b   Amadio, Anthony ^a,b   Antonovski, Victorio ^a,b   Petersen, Eric ^a,b  

^a UNIVERSITY OF CENTRAL FLORIDA   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DROPLET VAPORIZATION; OXIDIZERS; ROCKET INJECTORS;

DROPS; LIQUID PROPELLANTS; MACHINE DESIGN; PRESSURE EFFECTS; SHOCK WAVES; SUPERCRITICAL FLUIDS; SYSTEM STABILITY; THERMAL EFFECTS; VAPORIZATION;

ROCKETS;

EID: 34249033003     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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