Advanced Chemical Propulsion Study
- Author:
- Byers, Dave
- Published:
- October 27, 2004.
- Physical Description:
- 1 electronic document
- Additional Creators:
- Krebsbach, Al, Woodcock, Gordon, and Alexander, Leslie A.
Online Version
- hdl.handle.net , Connect to this object online.
- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access - Summary:
- A study was performed of advanced chemical propulsion technology application to space science (Code S) missions. The purpose was to begin the process of selecting chemical propulsion technology advancement activities that would provide greatest benefits to Code S missions. Several missions were selected from Code S planning data, and a range of advanced chemical propulsion options was analyzed to assess capabilities and benefits re these missions. Selected beneficial applications were found for higher-performing bipropellants, gelled propellants, and cryogenic propellants. Technology advancement recommendations included cryocoolers and small turbopump engines for cryogenic propellants; space storable propellants such as LOX-hydrazine; and advanced monopropellants. It was noted that fluorine-bearing oxidizers offer performance gains over more benign oxidizers. Potential benefits were observed for gelled propellants that could be allowed to freeze, then thawed for use.
- Other Subject(s):
- Collection:
- NASA Technical Reports Server (NTRS) Collection.
- Note:
- Document ID: 20050009897.
36th Annual Division for Planetary Science; 8-10 Nov. 2004; Louisville, KY; United States. - Terms of Use and Reproduction:
- No Copyright.
View MARC record | catkey: 15964232