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.

Subject Categories:

  • Combustion and Ignition
  • Rocket Engines
  • Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE