1 option
Liquid Oxygen/Liquid Methane Rocket Engine Development XCOR Aerospace
- Format:
- Conference/Event
- Author/Creator:
- DeLong, Dan, author.
- Conference Name:
- Aerospace Technology Conference & Exposition (2007-09-17 : Los Angeles, California, United States)
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 2007
- Summary:
- Because of low toxicity and low reactivity, methane and oxygen are identified as "green propellants", and have the highest performance (as measured in ISP) of any practical rocket propellants, except oxygen/hydrogen. Investigation into green propellant rocket engines identified liquid oxygen (LOX)/methane (CH4) as an excellent candidate for upper stage applications. This paper discusses work in LOX/CH4 engine development carried out by XCOR Aerospace, Incorporated
- Notes:
- Vendor supplied data
- Publisher Number:
- 2007-01-3876
- Access Restriction:
- Restricted for use by site license
The Penn Libraries is committed to describing library materials using current, accurate, and responsible language. If you discover outdated or inaccurate language, please fill out this feedback form to report it and suggest alternative language.