A New Approach for Single Stage Ascent to Orbit Silane Fuel in a New Vehicle Design

2005-01-3413

10/03/2005

Event
Aerospace Technology Conference and Exposition
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/2005-01-3413
Pages
8
Citation
Padanyi-Gulyas, D., and Bodo, A., "A New Approach for Single Stage Ascent to Orbit Silane Fuel in a New Vehicle Design," SAE Technical Paper 2005-01-3413, 2005, https://doi.org/10.4271/2005-01-3413.
Additional Details
Publisher
Published
Oct 3, 2005
Product Code
2005-01-3413
Content Type
Technical Paper
Language
English