Project Icarus: Preliminary Thoughts on the Selection Ofjbis, Probes Vol

Project Icarus: Preliminary Thoughts on the Selection Ofjbis, Probes Vol

Project Icarus: Preliminary Thoughts on the Selection ofJBIS, Probes Vol. and 69, Instruments... pp.4-10, 2016 PROJECT ICARUS: PRELIMINARY THOUGHTS ON THE SELECTION OF PROBES AND INSTRUMENTS FOR AN ICARUS-STYLE INTERSTELLAR MISSION I. A. CRAWFORD Department of Earth and Planetary Sciences, Birkbeck College London, Malet Street, London, WC1E 7HX, UK. In this paper we outline the range of probes and scientific instruments that will be required for an Icarus-style interstellar mission to fulfill its scientific objectives of exploring a nearby star, its attendant planetary system, and the intervening interstellar medium. Based on this preliminary analysis, we estimate that the minimum total Icarus scientific payload mass will be in the region of 100 tonnes. Of this, approximately 10 tonnes would be allocated for cruise-phase science instruments (not all of which would necessarily need to be decelerated at the target system), and about 35 tonnes would be contributed by the intra-system science payload itself (i.e. the dry mass of the stellar and planetary probes and their instruments). The remaining ~55 tonnes is allocated for the sub-probe intra-system propulsion requirements (crudely estimated from current Solar System missions; detailed modelling of sub-probe propulsion systems will be needed to refine this figure). However, the overall mass contributed by the science payload to the total that must be decelerated from the interstellar cruise velocity will be significantly more than 100 tonnes, as allowance must be made for the payload structural and infrastructural elements required to support, deploy, and communicate with the science probes and instruments. Based on the earlier Daedalus study, we estimate another factor of two to allow for these components. Pending the outcome of more detailed studies, it therefore appears that an overall science-related payload mass of ~200 tonnes will be required. This paper is a submission of the Project Icarus Study Group. Keywords: Interstellar travel, exoplanets, interstellar medium, stellar properties, planetary science, astrobiology 1. INTRODUCTION The Project Icarus study [1, 2] is tasked with designing an 2. TOP-LEVEL SCIENTIFIC OBJECTIVES interstellar space vehicle capable of making in situ scientific investigations of a nearby star and its accompanying planetary As discussed by Crawford [3], and building on earlier work system. This paper presents an initial consideration the range of by Webb [4] in the context of the Daedalus study, the Project probes and scientific instruments that will be required in order Icarus science objectives include: for Project Icarus to fulfill its scientific mission. It is important (1) Science to be conducted on route. This includes studies to realize that at this stage in the project any such analysis can of the interstellar medium (ISM) encountered traversed only be very preliminary, as decisions regarding the actual on the way to the target star, and also physical and complement of scientific instruments carried by an interstellar astrophysical studies which can make use of the Icarus mission will depend on the following: vehicle as an observing platform; (i) The available mass, power, and communication (2) Astrophysical studies of the target star itself, or stars, if bandwidth budgets; and a multiple system is selected; (ii) The architecture of the target star and planetary system (3) Planetary science studies of any planets in the target system, (especially the number and type of planets present, including moons and large asteroids of interest; and including any observations of possible biosignatures (4) Astrobiological/exobiological studies of any habitable that may have been made by solar system-based (or inhabited) planets which may be found in the target astronomical observations). planetary system. For the purposes of the Icarus project, it is expected that These broad science areas may themselves be sub-divided understanding of (i) will mature as the design progresses, into a number of different areas of investigation. These are whereas (ii) will be satisfied by the definition of a summarised in Table 1. hypothetical, but plausible, planetary system at a later stage of the project. The remaining sections of this paper outline the kinds, and approximate numbers, of sub-probes and accompanying Although neither of these key prerequisites are currently instruments that would be required to address these different defined, it is nevertheless considered worthwhile at this scientific questions. stage of the project to identify at least the kinds of probes 3. SCIENCE PROBES AND INSTRUMENTS and instruments, and their approximate numbers, that would be required by an Icarus-type interstellar mission conducting 3.1 Science Conducted En Route an initial scientific investigation of a nearby exoplanetary system. The main scientific investigations to be conducteden route will 1 I.A. Crawford TABLE 1: Preliminary List of Icarus Science Objectives. Scientific Area Area of Investigation Examples 1. Science en- route Outer solar system studies Heliosphere, Kuiper belt and Oort Cloud Local interstellar medium Structure, density, temperature, composition, magnetic fields, etc Astronomical studies Parallax measurements; other? Fundamental physics Gravitational waves, gravity, dark matter, etc 2. Stellar astrophysics Outer environment of target star Astrosphere, dust disk, comets, etc Target star astrophysics I Mass, composition, temperature, mag. fields Target star astrophysics II Photospheric and coronal activity; long-term monitoring Target star astrophysics III Stellar wind/corona composition 3. Planetary science Terrestrial planets I Mass, density, magnetic fields Terrestrial planets II Atmospheric composition and structure Terrestrial planets III Surface geology Terrestrial planets IV Internal structure (geophysics) Giant planets I Mass, density, magnetic fields Giant planets II Atmospheric composition and structure Asteroids/small bodies I Numbers, mass, density, composition Asteroids/small bodies II In situ dating of primitive meteorites 4. Astrobiology Astrobiology I Identification of habitable environments in target system Astrobiology II Search for biomarkers Astrobiology III Detection of planetary surfaces Astrobiology IV Life detection below planetary surfaces Astrobiology V Search for evidence of extinct life Astrobiology VI Biochemical characterization of extant life forms Astrobiology VII Search for evidence of technological artefacts in target system be studies of the interstellar medium (ISM) between the Sun heliosphere, Kuiper Belt and Oort Cloud as possible targets and the target star system. The sizes, physical properties, and for investigation. These three areas of investigation are rather locations of the low-density cloudlets known to be present in different. The instrumentation described above for the study the vicinity of the Sun, and the nature of the lower density inter- of the ISM will also be sufficient for heliospheric studies, and cloudlet medium, are of particular interest [5]. Key instruments indeed the boundary between the heliosphere and the local for these studies would be: ISM is of compelling scientific interest [5]. However, it is not considered here that Kuiper belt objects (KBO) should be a high • A dust analyser (to determine both dust masses and priority for Icarus, partly because pre-Icarus precursor missions compositions) are likely to have made in situ observations of these objects, • Gas analyser(s) (to measure densities, ionisation states, and partly because refining the Icarus trajectory to pass close a and composition of the gas phase interstellar medium – KBO may overly complicate the flight profile. The Oort cloud is probably a suite of several instruments in practice) so thinly populated that it is unlikely that Icarus will pass close • Magnetometer(s) and plasma wave instruments enough to an Oort cloud comet to make in situ observations, • High-energy particle (cosmic ray) detectors and in any case the vehicle will probably be travelling at or close to its cruise velocity, making such observations difficult The instruments required to study the structure of the (and potentially dangerous). interstellar medium should have the highest priority for cruise- phase science. These instruments would be similar to those 3.2 Studies of Target Star(s) routinely flown on outer Solar System missions (e.g. Cassini; [6]) and proposed for interstellar precursor missions (e.g. [7]). Studies of the target star(s) will be of compelling astrophysical They could be mounted on the main vehicle, but booms (or free- interest. However, it must be noted that for these very nearby flying sub-probes) may be desirable to insulate them as much as stars a lot can, and will, be learned from astronomical possible from electromagnetic and other interference from the observations made from Earth. It follows that in situ studies vehicle. Thought will also have to be given to protection from should be designed to complement these astronomical studies, interstellar dust impacts. and be used to obtain information that cannot plausibly be obtained using telescopic observations from the Solar System. If Project Icarus is also to be used as a platform for Examples include in situ measurements of stellar wind and detecting ‘exotic’ (e.g. dark matter) particles then additional magnetic field, high-spatial resolution observations of stellar instrumentation may be required. The Alpha Magnetic photospheres, active regions and coronae, and ultra-high

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