Additional Fuel Component Application for Hydrogen Scramjet Boosting Central Institute of Aviation Motors

Format:

Conference/Event

Author/Creator:

Rudakov, A. S., author.

Conference Name:

Aerospace Atlantic Conference & Exposition (1990-04-23 : Dayton Oh, Ohio, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1990

Summary:

AbstractThe results of computational investigations carried out to clarify the possibilities of hydrogen scramjet thrust uprating in hypersonic flight (Mf>8) by adding to the fuel substances with higher density are presented. Thrust, specific impulse and density impulse are calculated while adding nitrogen, oxygen, water or inert liquated gases. For scramjet boosting in hypersonic flight it is suggested to add oxygen or a heavy inert gas to stoichiometric part of hydrogen instead of excessive part of hydrogen

Notes:

Vendor supplied data

Publisher Number:

900990

Access Restriction:

Restricted for use by site license