Specific impulse
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The concept Specific impulse represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
The Resource
Specific impulse
Resource Information
The concept Specific impulse represents the subject, aboutness, idea or notion of resources found in University of Missouri-St. Louis Libraries.
- Label
- Specific impulse
- Source
- nasat
27 Items that share the Concept Specific impulse
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- Trajectory optimization of an interstellar mission using solar electric propulsion : final report for NASA grant NAG3-1731
- Advanced low-cost O[subscript 2]/H[subscript 2] engines for the SSTO application
- An analytic approximation to very high specific impulse and specific power interplanetary space mission analysis
- Analysis of 100-lb[subscript f] (445-N) LO2-LCH4 reaction control engine impulse bit performance
- Analysis of a rocket based combined cycle engine during rocket only operation
- Application of the NEXT ion thruster lifetime assessment to thruster throttling
- Beamed-energy propulsion (BEP) study
- Benefits of low-power electrothermal propulsion
- Benefits of low-power electrothermal propulsion
- COMPASS final report : Radioisotope Electric Propulsion (REP) centaur orbiter new frontiers mission
- Design of a power management and distribution system for a thermionic-diode powered spacecraft
- Design of a power management and distribution system for a thermionic-diode powered spacecraft
- Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure
- High-power ion thruster technology
- Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion
- Integrity of the plasma magnetic nozzle
- Ion engine and hall thruster development at the NASA Glenn Research Center
- Mission advantages of constant power, variable ISP electrostatic thrusters
- Mission advantages of constant power, variable Isp electrostatic thrusters
- NASA's Evolutionary Xenon Thruster (NEXT) Prototype Model 1R (PM1R) ion thruster and propellant management system wear test results
- Operational characteristics of the SPT-140 Hall thruster
- Performance of a FAKEL K10K resistojet
- Performance of an axisymmetric rocket based combined cycle engine during rocket only operation using linear regression analysis
- Scaling of ion thrusters to low power
- Status of the NEXT ion thruster Long Duration Test
- The diagnostics of the external plasma for the plasma rocket : final report, NASA Graduate Student Researchers Program, Johnson Space Center, contract number--NGT9-5
- The effect of magnetohydrodynamic (MHD) energy bypass on specific thrust for a supersonic turbojet engine
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.umsl.edu/resource/BqRXriUNKEc/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.umsl.edu/resource/BqRXriUNKEc/">Specific impulse</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.umsl.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.umsl.edu/">University of Missouri-St. Louis Libraries</a></span></span></span></span></div>
