Novel mission concepts for polar coverage : An overview of recent developments and possible future applications

The paper provides a survey of novel mission concepts for continuous, hemispheric polar observation and direct-link polar telecommunications. It is well known that these services cannot be provided by traditional platforms: geostationary satellites do not cover high-latitude regions, while low- and medium-orbit Sun-synchronous spacecraft only cover a narrow swath of the Earth at each passage. Concepts that are proposed in the literature are described, including the pole-sitter concept (in which a spacecraft is stationary above the pole), spacecraft in artificial equilibrium points in the Sun–Earth system and non-Keplerian polar Molniya orbits. Additionally, novel displaced eight-shaped orbits at Lagrangian points are presented. For many of these concepts, a continuous acceleration is required and propulsion systems include solar electric propulsion, solar sail and a hybridisation of the two. Advantages and drawbacks of each mission concept are assessed, and a comparison in terms of high-latitude coverage and distance, spacecraft mass, payload and lifetime is presented. Finally, the paper will describe a number of potential applications enabled by these concepts, focusing on polar Earth observation and telecommunications.

[1]  Nm Wallace Testing of the Qinetiq T6 Thruster in Support of the ESA BepiColombo Mercury Mission for the ESA BepiColombo Mission , 2004 .

[2]  Colin R. McInnes,et al.  Generation of Optimal Trajectories for Earth Hybrid Pole Sitters , 2011 .

[3]  Johnie M. Driver Analysis of an Arctic Polesitter , 1979 .

[4]  Colin R. McInnes,et al.  Systems design of a hybrid sail pole-sitter , 2011 .

[5]  Colin R. McInnes,et al.  Periodic Orbits Above the Ecliptic in the Solar-Sail Restricted Three-Body Problem , 2007 .

[6]  Alessandro Antonio Quarta,et al.  Parametric model and optimal control of solar sails with optical degradation , 2006 .

[7]  David Folta,et al.  Unique Non-Keplerian Orbit Vantage Locations for Sun-Earth Connection and Earth Science Vision Roadmaps , 2001 .

[8]  P. G. Kazantzis Numerical determination of families of three-dimensional double-symmetric periodic orbits in the restricted three-body problem. I. , 1979 .

[9]  Robert L. Forward,et al.  Statite - A spacecraft that does not orbit , 1991 .

[10]  David M. Murphy,et al.  Scalable Solar-Sail Subsystem Design Concept , 2003 .

[11]  James R. Wertz,et al.  Space Mission Analysis and Design , 1992 .

[12]  Malcolm Macdonald,et al.  Extension of the Molniya orbit using low-thrust propulsion , 2011 .

[13]  Colin R. McInnes,et al.  Artificial Three-Body Equilibria for Hybrid Low-Thrust Propulsion , 2008 .

[14]  Emmanuel Trélat,et al.  Eight-shaped Lissajous orbits in the Earth-Moon system , 2011 .

[15]  Pamela G. Anderson,et al.  Extension of earth orbits using low-thrust propulsion , 2010 .

[16]  Alex Coletti,et al.  The possibilities of polar meteorology, environmental remote sensing, communications and space weather applications from Artificial Lagrange Orbit , 2011 .

[17]  Les Johnson,et al.  NanoSail-D: A solar sail demonstration mission , 2011 .

[18]  Colin R. McInnes,et al.  Solar sail parking in restricted three-body systems , 1994 .

[19]  Colin R. McInnes,et al.  Solar Sailing: Technology, Dynamics and Mission Applications , 1999 .