- High
Power Electric Propulsion (
HiPEP) is a
variation of ion
thruster for use in
nuclear electric propulsion applications. It was ground-tested in 2003...
- currently[clarification needed]
working on a 20–50 kW
electrostatic ion
thruster called HiPEP which will have
higher efficiency,
specific impulse, and a
longer lifetime...
-
Nuclear Electric Xenon Ion
System (NEXIS) High
Power Electric Propulsion (
HiPEP), 25 kW, test
example built and run
briefly on the
ground EADS Radio-frequency...
-
proven ion
engine designs such as NASA's High
Power Electric Propulsion (
HiPEP)
operated at 80%
total thruster/PPU
energy efficiency. On 24
October 2008...
-
electrodes HiPEP –
using positive ions as the propellant,
created using microwaves Radiofrequency ion
thruster –
generalization of
HiPEP Hall-effect...
-
propulsion devices for
spacecraft propulsion,
where a
broad range of
devices (
HiPEP, some ion thrusters, or
electrodeless plasma thrusters),[citation needed]...
-
Gridded ion
thruster NASA
Solar Technology Application Readiness (NSTAR)
HiPEP Radiofrequency ion
thruster Hall-effect thruster,
including its subtypes...
-
HiPEP ion
engine test (2003)...
- Patterson, M. (July 2004). "An
Overview of the High
Power Electric Propulsion (
HiPEP) Project". 40th AIAA/ASME/SAE/ASEE
Joint Propulsion Conference and Exhibit...
- creation,
scientists successfully tested a High
Power Electric Propulsion (
HiPEP) ion engine,
which offered substantial advantages in fuel efficiency, thruster...
