[PDF] Top 20 Small-body encounters using solar sail propulsion
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Small-body encounters using solar sail propulsion
... of solar sail propulsion due to their high-energy require- ...enabled using current solar sail technology, with a large enough sail, that would have resulted in a 68% ... See full document
11
Extension of Earth-Moon libration point orbits with solar sail propulsion
... the solar sail induced acceleration, families of Lyapunov, halo, ver- tical Lyapunov, Earth-centred, and distant retrograde orbits are ...the solar sail circular restricted three-body ... See full document
20
Solar sail periodic orbits in the Earth-Moon three-body problem
... of solar sailing lies in the fact that, contrary to other low-thrust propulsion technologies like electric propulsion, it does not rely on an on-board propellant ...by solar photons impinging ... See full document
11
Hybrid solar sail and SEP propulsion for novel Earth observation missions
... two propulsion systems complement each other, cancelling their reciprocal disadvantages and ...the sail cannot ...auxiliary solar sail provides part of the acceleration, enabling saving of ... See full document
13
Artificial halo orbits for low-thrust propulsion spacecraft
... a solar sail low-thrust propulsion system, but only in certain allowed ...the sail lightness number and sail ...the solar-sail three body ...the ... See full document
16
Hybrid solar sail and SEP propulsion for novel Earth observation missions
... two propulsion systems complement each other, cancelling their reciprocal disadvantages and ...the sail cannot ...auxiliary solar sail provides part of the acceleration, enabling saving of ... See full document
14
New periodic orbits in the solar sail restricted three body problem
... We follow the conventions set out in McInnes. 1 We consider a rotating coor- dinate system in which the primary masses are fixed on the x-axis with the origin at the centre of mass, the z-axis is the axis of rotation and ... See full document
11
Technology requirements of exploration beyond Neptune by solar sail propulsion
... post sail jettison the probe will continue to ...the sail is attached to the IHP and for which a 10-m central cutout is provided in the sail ...the solar sail pointing requirements are ... See full document
36
Displaced periodic orbits with low-thrust propulsion
... and solar electric technology provide alternative forms of space- craft ...These propulsion systems can enable exciting new space-science mission concepts such as solar system exploration and deep ... See full document
15
Displaced geostationary orbit design using hybrid sail propulsion
... chemical propulsion system, the performance of impulsive control was found to be very ...Even small displacements of 35 km, the minimum to rise above the geostationary station keeping box, could not be ... See full document
41
Non-Keplerian orbits using hybrid solar sail propulsion for Earth applications
... hybrid propulsion, ...lifetime using these maximised injected ...the solar arrays and a slightly smaller sail size since the sail area does not include the area of the thin film ... See full document
275
Optimal solar sail interplanetary heteroclinic transfers for novel space applications
... a solar sail acceleration and fixing the attitude of the solar sail with re- spect to the Sun-sail line, intersections between restricted three-body models were found on suitable ... See full document
37
Designing displaced lunar orbits using low-thrust propulsion
... of solar electric propulsion (SEP) technology is now a realistic option for designing trajectories for interplanetary missions, while solar sail technology is currently under ...third ... See full document
11
New periodic orbits in the solar sail three-body problem
... X ∗ (0) = X(0) + (I − M ) −1 [X(T ) − X(0)] (13) where X ∗ (0) is the improved initial condition and M is the monodromy matrix. One of the problems encountered with this Newton method is that the determinant of (I − M ) ... See full document
12
Solar sail equilibria in the elliptical restricted three-body problem
... the small eccentricity ...in small eccentricity systems, even although exact out-of-plane equilibria do not exist for the general elliptical restricted three-body ...three- body system have ... See full document
27
Analytical three-phase transfer to a solar polar orbit using solar sail propulsion
... the sail angle in the first phase ...a small sail angle in the first ...of sail angles can be identified for which the trip time is ... See full document
7
Solar sail dynamics in the three-body problem: homoclinic paths of points and orbits
... The linear solutions given in the previous section will only closely approximate the motion of the sail given in (1) for small amplitudes. For larger amplitude periodic orbits, we have two options: ... See full document
13
Low-thrust enabled highly non-Keplerian orbits in support of future Mars exploration
... and solar sail low thrust propulsion systems have their own advantages and ...disadvantages. Solar sailing has the advantage that it requires no propellant, and thus can maintain continuous ... See full document
38
Control of Lagrange point orbits using solar sail propulsion
... of propulsion which utilises solar radiation pressure to provide a useful ...The sail is a thin reflective film with a thickness of order 2 μm, with a large reflective area in order to intercept a ... See full document
11
Solar sail mission applications and future advancement
... chemical propulsion for the IHP mission appears unattractive from this concept, however should a specific impulse of over 450 seconds be achieved then such a variant, with a large burn at 4 solar radius may ... See full document
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