[PDF] Top 20 Extension of Martian orbits using continuous low-thrust propulsion
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Extension of Martian orbits using continuous low-thrust propulsion
... These orbits use continuous out-of-plane acceleration to allow the ascending node angle to rotate to match the motion of the mean Sun, giving the Sun-synchronous ... See full document
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Extension of highly elliptical Earth orbits using continuous low-thrust propulsion
... The extension of highly elliptical orbits, with free selection of orbit period, using low- thrust propulsion is ...proposed orbits, termed Taranis orbits, are ... See full document
36
Survey of highly non-Keplerian orbits with low-thrust propulsion
... Keplerian orbits from the larger sets of non-Keplerian orbits (NKOs) and natural Keplerian orbits is ...such orbits is given, tracing the field from its roots to current ...non-Keplerian ... See full document
54
Extension of low-thrust propulsion to the autonomous coplanar circular restricted four body problem with application to future Trojan Asteroid missions
... a low-thrust ...of continuous low-thrust propulsion) equilibrium solutions are identified, that have the potential to be exploited in future science ...zero thrust, there ... See full document
12
Extension of the Molniya orbit using low-thrust propulsion
... orbit using low-thrust propulsion is ...elliptical orbits are enabled by existing low-thrust propulsion technology, enabling new Earth Observation science and ... See full document
20
Sun-synchronous highly elliptical orbits using low-thrust propulsion
... any low-thrust ...all orbits in ...an extension of this solution, and are only enabled through the use of continuous ...maximum thrust of 478 mN is required, which will decrease ... See full document
15
Static highly elliptical orbits using hybrid low-thrust propulsion
... two propulsion systems enables a new range of missions in which continuous low-thrust is ...geostationary orbits (GEO) displaced above or below the equatorial plane to create new ... See full document
34
Artificial halo orbits for low-thrust propulsion spacecraft
... the low-thrust acceleration directed towards sunward are shown to be feasible with such low-thrust ...constant continuous low-thrust acceleration, to produce closed ... See full document
16
Novel orbits of Mercury and Venus enabled using low-thrust propulsion
... novel orbits of both Mercury and Venus to enhance the opportunities for remote ...sensing. Continuous low-thrust propulsion is used to extend the critical inclination of highly ... See full document
21
Static highly elliptical orbits using hybrid low-thrust propulsion
... elliptical orbits, termed Taranis orbits, is considered for continuous observation of high latitude ...regions. Low-thrust propulsion is used to alter the critical inclination of ... See full document
22
Static highly elliptical orbits using hybrid low-thrust propulsion
... enable continuous observation of frigid and neighboring temperate ...Taranis orbits have been considered using Solar Electric Propulsion (SEP), a mature technology with a high Technology ... See full document
35
Non-Keplerian orbits using low thrust, high ISP propulsion systems
... constrained propulsion systems such as SEP, be equally applied to the Lagrange points of Planet-Sun systems as well as those of Moon-Planet ...constrained propulsion systems, such as solar sailing, the ... See full document
15
Novel orbits of Mercury, Venus and Mars enabled using low-thrust propulsion
... elliptical orbits are considered, two conditions can be combined to obtain sun-synchronous ...These orbits use continuous out-of-plane acceleration to allow the ascending node angle to rotate to ... See full document
26
Extension of the proximity-quotient control law for low-thrust propulsion
... In general, NEO deflection techniques fall into four broad categories [7]: kinetic impacts, propulsive devices, induced changes to the asteroid surface, and ablation devices. A previous study by the authors compared the ... See full document
10
Design of optimal Earth pole-sitter transfers using low-thrust propulsion
... temporal resolution that nowadays can be obtained comes from satellites in geostationary orbit (GEO), but it is well known that high latitude regions are out of sight for GEO spacecraft. Recent studies are therefore ... See full document
27
Displaced non-Keplerian orbits using impulsive thrust
... of continuous low thrust propulsion to generate artificial equilibria was apparently first proposed by Dusek (1966) who pointed out that a spacecraft could be held at an artificial equilibrium ... See full document
35
Displaced geostationary orbits using hybrid low-thrust propulsion
... spacecraft propulsion system to maintain displaced NKOs [2, 4, 7- 8, ...a continuous, propellant-less thrust ...primary propulsion system on a reasonable sized mission is still rather ...a ... See full document
29
Displaced periodic orbits with low-thrust propulsion
... spacecraft propulsion which can enable exciting new space-science mission concepts such as solar system ex- ploration and deep space ...of propulsion can provide energy changes greater than are possible ... See full document
15
Extension of earth orbits using low-thrust propulsion
... The Molniya orbit is a type of highly elliptical orbit, with a period, typically, of one half of a sidereal day, characteristic of the Molniya orbit is the fixed 63.4deg or 116.6deg inclination [3]. At either of these ... See full document
13
Multi-objective optimisation of constellation deployment using low-thrust propulsion
... constellation using low-thrust ...(which low- thrust trajectory is required to achieve the required slot) that can provide maximum pay-off, minimum launch cost and minimise the mass of ... See full document
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