The NASA Astrobiology Roadmap

The NASA Astrobiology Roadmap provides guidance for research and technology development across the NASA enterprises that encompass the space, Earth, and biological sciences. The ongoing development of astrobiology roadmaps embodies the contributions of diverse scientists and technologists from government, universities, and private institutions. The Roadmap addresses three basic questions: How does life begin and evolve, does life exist elsewhere in the universe, and what is the future of life on Earth and beyond? Seven Science Goals outline the following key domains of investigation: understanding the nature and distribution of habitable environments in the universe, exploring for habitable environments and life in our own solar system, understanding the emergence of life, determining how early life on Earth interacted and evolved with its changing environment, understanding the evolutionary mechanisms and environmental limits of life, determining the principles that will shape life in the future, and recognizing signatures of life on other worlds and on early Earth. For each of these goals, Science Objectives outline more specific high-priority efforts for the next 3-5 years. These 18 objectives are being integrated with NASA strategic planning.     

Regulatory Compliance-The Real World

An introduction to the real world of product safety liaison. As the ``World Market' matures, the stature of the safety liaison process increases in importance. Means for accelerating the regulatory process are detailed and pertinent standards are identified. The redesign of a domestic switching power supply to ``World Standards' is described.     

Integrating Avionics in the Conceptual Design Phase

The avionics components of modern military aircraft significantly impact the cost and effectiveness of the total aeronautical system. In the early conceptual phase, aeronautical system designers give scant attention to designing the avionics components. The design team generally provides weight, volume and power considerations for the desired avionics functions and assumes that an avionics suite can be assembled. Less than comprehensive attention is given to the interacting effect avionics have with the other system components. In contrast, the designers expend a very large effort on finding the best balanced combination of airframe and propulsion components which satisfy the design objectives. This paper shows why avionics must be a co-equal member of the aeronautical system along with airframe, propulsion, and armament. To become a co-equal partner, avionics must be an element of the system design iterations and analysis commencing with the early conceptual design phase of a new aeronautical system.     

Not the sons of Adam : Religious responses to ETI

Christianity, Judaism and Islam share certain preconceptions, among them an adherence to the idea of man created in the image of God. This article examines the responses of religious experts in these religions to the possibility of contact with ETI. Responses from religious experts of varying branches in all three of these religions suggest that even within a given religion a number of paradigms could emerge in response to possible ETI contact. Some of the factors that might affect responses within each religion are examined.     

Energy release in double layers

A Double layer (DL) in a current carrying plasma sustains a localised net potential difference and acts as an impedance converting electrical energy to directed particle energy determined by the DL potential. DL's accelerate equal numbers of ions and electrons for relativistic energies, otherwise electron energisation predominates. Their time independent structure may be described as a BGK (Bernstein-Greene-Kruskal) state analogous to that for laminar shocks, and certain existence criteria must be satisfied. The generalised Langmuir criterion requires total particle pressure balance over the DL and may imply propagation in the plasma reference frame. The Bohm criteria require sufficiently large current densities and are closely related to the local stability condition at the edges of the DL. The DL potential must be sustained externally, for example by the release of stored magnetic energy. A steady state is also possible where (externally maintained) mass motions drive a dynamo region connected by currents to the DL which acts as an electrical load.     

Earth weather and climate control: can space technology contribute?

With ongoing progress in space technology, questions of its potential for the modification of weather and climate phenomena (often summarized by the term ‘geoengineering’) ranging from small-scale severe weather events to mitigation of effects caused by global climate change and ozone depletion have become popular. This paper reviews the current state of scientifically based studies in this context and attempts to provide a basis for an assessment of geoengineering efforts with respect to technological, economic and fundamental scientific aspects. The overview indicates that the current state of knowledge about climate variability as a consequence of natural and anthropogenic influences is sufficient to classify geoengineering solutions as highly risky and their consequences as extremely difficult to predict. Even on smaller scales and with less complexity of interacting processes, only very limited boundary conditions, i.e. a narrow range of atmospheric variability and land surface topography favouring the intended alteration, seem to justify weather modification. Moreover, as for systems reaching scales of large organized storms and hurricanes, required energy and control resources are well beyond existing capabilities. Consequently, the use of space technology for provision of better information on environmental change and integration of remote sensing data into weather and climate models forecasts is supported.     

Fourier parameters of heliospheric current sheet and their significance

If the path of the neutral line on the coronal source surface is expressible as a singlevalued function (colatitude vs longitude ), then Fourier analysis of ctn with respect to leads to a simple algorithm for realistically mapping the neutral line outward to model the heliospheric current sheet (HCS) at distancesr1 AU. To be compatible with MHD, the source surface used for this mapping should be prolate (aligned with dipole axis) rather than spherical. Orientation of the Sun's magnetic-dipole moment is indicated by them=1 Fourier amplitude (a ₁ sin +b ₁ cos ) of ctn on the source surface. Physical features (including the neutral line) on a prolate source surface intrinsically map to lower dipole latitudes atr1 AU in the heliosphere, and Ulysses observations of a unipolar field at latitudes beyond 30°S (when the neutral line on the source surface still reached 39°S) confirm the expected geometry.     

Non-destructive sampling of a comet

The boundary conditions for a non-destructive sample acquisition system are outlined and the development of a new robotic sampling system suited for use on a cometary surface is briefly discussed. Additionally we present some new results on strength and deformation behaviour of synthetic cometary analogue material.