A theoretical treatment of technical risk in modern propulsion system design
Main Author: | Roth, Bryce Alexander |
---|---|
Format: | Others |
Language: | en_US |
Published: |
Georgia Institute of Technology
2006
|
Subjects: | |
Online Access: | http://hdl.handle.net/1853/12221 |
Similar Items
-
Survey of developments of ionic propulsion systems for space vehicles
by: Hungerford, Franklin McDonald, 1929-
Published: (1962) -
A technique for rapid prediction of aftbody nozzle performance for hypersonic launch vehicle design
by: Bradford, John Edward
Published: (2006) -
Simulation of direct current microdischarges for microthruster applications
by: Kothnur, Prashanth Srinivasa
Published: (2008) -
Electric Propulsion and Controller Design for Drag-Free Spacecraft Operation in Low Earth Orbit
by: Marchetti, Paul J
Published: (2006) -
A novel numerical analysis of Hall Effect Thruster and its application in simultaneous design of thruster and optimal low-thrust trajectory
by: Kwon, Kybeom
Published: (2010)