Suggested Topics within your search.
Suggested Topics within your search.
- Specific impulse
- Electric propulsion 7
- High impulse 7
- Propulsion system performance 7
- Ion engines 6
- Xenon 6
- Rocket engines 5
- Rocket thrust 5
- Low Earth orbits 4
- Propulsion system configurations 4
- Resistojet engines 4
- Geosynchronous orbits 3
- Performance tests 3
- Propellants 3
- Rocket engine design 3
- Rocket nozzles 3
- Space vehicles 3
- Thermodynamic cycles 3
- Arc jet engines 2
- Electrostatic propulsion 2
- Energy conversion 2
- Hall thrusters 2
- Hypersonic flight 2
- Ion propulsion 2
- Liquid rocket propellants 2
- Low thrust 2
- Magnetic fields 2
- Management systems 2
- Mission planning 2
- Plasma propulsion 2
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1
Benefits of low-power electrothermal propulsion /
Published 1997Connect to online resource:
Online Access
Online Access
Government Document eBook -
2
Ion engine and hall thruster development at the NASA Glenn Research Center /
Published 2002Online Access
Online Access
Government Document eBook -
3
Mission advantages of constant power, variable ISP electrostatic thrusters
Published 2000Government Document Microfilm Book -
4
Integrity of the plasma magnetic nozzle
Published 2009Connect to online resource
Connect to online resource
Government Document Electronic eBook -
5
Status of the NEXT ion thruster Long Duration Test
Published 2005Connect to online resource
Connect to online resource
Government Document Electronic Conference Proceeding eBook -
6
NASA's Evolutionary Xenon Thruster (NEXT) Prototype Model 1R (PM1R) ion thruster and propellant management system wear test results
Published 2010Connect to online resource
Connect to online resource
Government Document Electronic Conference Proceeding eBook -
7
Application of the NEXT ion thruster lifetime assessment to thruster throttling
Published 2010Connect to online resource
Connect to online resource
Government Document Electronic Conference Proceeding eBook -
8
The effect of magnetohydrodynamic (MHD) energy bypass on specific thrust for a supersonic turbojet engine
Published 2010Connect to online resource
Connect to online resource
Government Document Electronic Conference Proceeding eBook -
9
COMPASS final report Radioisotope Electric Propulsion (REP) centaur orbiter new frontiers mission /
Published 2011Online Access
Online Access
Government Document Electronic eBook -
10
Beamed-energy propulsion (BEP) study
Published 2012Online Access
Online Access
Government Document Electronic eBook -
11
Performance and endurance tests of a multipropellant resistojet for space station auxiliary propulsion
Published 1986Government Document Microfilm Book -
12
Analysis of 100-lb[subscript f] (445-N) LO₂-LCH₄ reaction control engine impulse bit performance
Published 2012Online Access
Government Document Electronic eBook -
13
Characteristics of ions emitted fron high-current hollow cathodes
Published 1994Government Document Microfilm Book -
14
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15
A low-erosion starting technique for high-performance arcjets
Published 1994Government Document Microfilm Book -
16
Advanced low-cost O₂/H₂ engines for the SSTO application
Published 1994Government Document Microfilm Book -
17
Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion /
Published 2012Online Access
Online Access
Government Document Conference Proceeding eBook -
18
Mission advantages of constant power, variable Isp electrostatic thrusters /
Published 2000Online Access
Online Access
Government Document eBook -
19
Operating characteristics of the Russian D-55 thruster with anode layer
Published 1994Government Document Microfilm Book -
20