Accession Number:
ADA409123
Title:
The Performance of a Hybrid Rocket With Swirling GOx Injection
Descriptive Note:
Conference paper
Corporate Author:
NATIONAL CHENG KUNG UNIV TAINAN (TAIWAN)
Personal Author(s):
Report Date:
2002-07-01
Pagination or Media Count:
8.0
Abstract:
With the developed HTPB curing process a 10-Kg thrust hybrid rocket was built and passed several static firing tests here in ASTRC. The motor was designed similar to the classical one with an aft-mixing chamber. The purpose of preset study is then to develop the enhancement mechanism for oxidizer and fuel vapor mixing and flame holding to assess the necessity of aft-mixing chamber that is usually employed in a classical hybrid rocket design.
Descriptors:
Subject Categories:
- Combustion and Ignition
- Rocket Engines
- Rocket Propellants