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Scaling of ion thrusters to low power
by Patterson, Michael J.
1998
Format: Book and Microform

✔ Available Joyner - Microforms B300

Call Number: NAS 1.15:206530

An analytic approximation to very high specific impulse and specific power interplanetary space mission analysis
by Williams, Craig Hamilton
1995
Format: Book and Microform

✔ Available Joyner - Microforms B300

Call Number: NAS 1.15:107058

Mission advantages of constant power, variable ISP electrostatic thrusters
by Oleson, Steven R. (Steven Robert), 1964-
2000
Format: Book and Microform

✔ Available Joyner - Microforms B300

Call Number: NAS 1.15:210477

Improving the total impulse capability of the NSTAR ion thruster with thick-accelerator-grid ion optics
by Soulas, George C. (George Chris), 1966-
2001
Format: Book and Microform

✔ Available Joyner - Microforms B300

Call Number: NAS 1.15:211276

Performance of a FAKEL K10K resistojet
by Jankovsky, Robert S.
1997
Format: Book and Microform

✔ Available Joyner - Microforms B300

Call Number: NAS 1.15:113127

Operational characteristics of the SPT-140 Hall thruster
1997
Format: Book and Microform

✔ Available Joyner - Microforms B300

Call Number: NAS 1.15:113162

Design of a power management and distribution system for a thermionic-diode powered spacecraft
by Kimnach, Greg L.
1996
Format: Book and Microform

✔ Available Joyner - Microforms B300

Call Number: NAS 1.15:107298

Operating characteristics of the Russian D-55 thruster with anode layer
by Sankovic, John M.
1994
Format: Book and Microform

✔ Available Joyner - Microforms B300

Call Number: NAS 1.15:106610

A low-erosion starting technique for high-performance arcjets
by Sankovic, John M.
1994
Format: Book and Microform

✔ Available Joyner - Microforms B300

Call Number: NAS 1.15:106627

Analysis of a rocket based combined cycle engine during rocket only operation
1998
Format: Book and Microform

✔ Available Joyner - Microforms B300

Call Number: NAS 1.15:206639/REV 1

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Scaling of ion thrusters to low power

An analytic approximation to very high specific impulse and specific power interplanetary space mission analysis

Mission advantages of constant power, variable ISP electrostatic thrusters

Improving the total impulse capability of the NSTAR ion thruster with thick-accelerator-grid ion optics

Performance of a FAKEL K10K resistojet

Operational characteristics of the SPT-140 Hall thruster

Design of a power management and distribution system for a thermionic-diode powered spacecraft

Operating characteristics of the Russian D-55 thruster with anode layer

A low-erosion starting technique for high-performance arcjets

Analysis of a rocket based combined cycle engine during rocket only operation

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