Combustion diagnosis for analysis of solid propellant rocket abort hazards: Role of spectroscopy

Solid rocket propellant plume temperatures have been measured using spectroscopic methods as part of an ongoing effort to specify the thermal-chemical-physical environment in and around a burning fragment of an exploded solid rocket at atmospheric pressures. Such specification is needed for launch s...

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Journal of physics. Conference series 2014-01, Vol.548 (1), p.12055-10
Hauptverfasser:	Gill, W, Cruz-Cabrera, A A, Donaldson, A B, Lim, J, Sivathanu, Y, Bystrom, E, Haug, A, Sharp, L, Surmick, D M
Format:	Artikel
Sprache:	eng
Schlagworte:	Combustion Droplets Fragmentation Launches Payloads Physics Propellants Rocket propellants Rockets Solid propellants Solid rocket propellants Soot Spectroscopy Spectrum analysis
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!