A New Approach for Single Stage Ascent to Orbit Silane Fuel in a New Vehicle Design Nitronics Aerospace Technologies, LLC

Format:

Conference/Event

Author/Creator:

Padanyi-Gulyas, David, author.

Conference Name:

Aerospace Technology Conference & Exposition (2005-10-03 : Grapevine, Texas, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2005

Summary:

Spacecraft designs incorporating a propulsion system powered by a more efficient fuel would greatly reduce the oxidizer to payload ratio. This could be accomplished with a single-stage vehicle that uses air while in the atmosphere and switches to onboard oxidizer only after reaching the upper limit of the atmosphere. In this presentation, a revolutionary new vehicle is proposed that incorporates silane-based fuels into an air-breathing spacecraft design that achieves orbit via low ascent angles, where it then switches to onboard oxidizer. A ceramic and alloy propulsion system takes advantage of the properties of silane, utilizing both the oxygen and the 80% nitrogen of the atmosphere for combustion

Notes:

Vendor supplied data

Publisher Number:

2005-01-3413

Access Restriction:

Restricted for use by site license