Advances in auroral imaging from space

Space imaging of the aurora provides unique quantitative information on the instantaneous global distribution and pattern of the aurora - a direct result of particle acceleration and precipitation processes occurring throughout the magnetosphere. Techniques for imaging from space have usually involved systematically scanning a detector across the earth using some combination of satellite motion and spin, scanning mirrors, and/or electronic scanning. The recent advent of CCD image sensor arrays opens up possibilities for vastly improved sensitivity and resolution in satellite imagers, although scanning systems retain significant advantages in situations where scattered light is a problem and where narrow band optical interference filters are needed.A new type of imaging instrument being built in Canada for the Swedish Viking satellite will employ a two-dimensional CCD array detector which is fibre-optically coupled to a micro-channel plate intensifier. It will produce images of low light level auroral emissions at the rate of one image per spin of the satellite (20 seconds). The instrument operates in the vacuum ultraviolet and uses a fast inverse Cassegrain optical system. Charge is shifted in the CCD imaging array in synchronism with the moving image so that exposure times of approximately one second will be achieved.     

Reactive control as a substrate for telerobotic systems

Reactive control, a recently emerged paradigm for guiding robots in unstructured and dynamic environments, and related work are reviewed. Pertinent telerobotics research for intelligent navigation is briefly surveyed. A scheme-based reactive control system that allows teleoperators to direct a mobile platform without undue concern for local obstacle avoidance is described. By using an analog of the potential field methodology, repulsive forces are constructed around nearby obstacles, allowing the robot to avoid them and enabling the telerobot operator to concentrate on the more global aspects of the mission. The structure for this paradigm enables real-time computation. The principles are extendible to manipulator operations. Results of robot simulation and experiments that demonstrate the concepts described are reported     

Direct evidence for chromospheric evaporation in a well-observed compact flare

We have observed the flare of 1980 May 7 1456 UT with several Solar Maximum Mission instruments, in coordination with the Sacramento Peak Observatory Vacuum Tower Telescope. From the X-ray data we determine the total amount of plasma at T > 2 × 10⁶ K, commonly attributed to chromospheric evaporation. From Hα we have determined the amount of plasma that has been evaporated from the chromosphere. We find that enough material has been evaporated from the chromosphere to account for the X-ray plasma. Taken together, the Hα, soft and hard X-ray images suggest that chromospheric evaporation is driven both by flare accelerated electrons, during the impulsive phase, and conduction, during the thermal phase.     

In situ and remote sensing of thermospheric winds during the energy budget campaign

This paper summarizes the dynamical information obtained in the lower thermosphere during the Energy Budget Campaign, by three experimental techniques: rocket-borne falling spheres instrumented with accelerometers and Tri-Methyl-Aluminium (TMA) trails, and from a ground-based Fabry-Perot interferometer. Winds of 200–400 m/sec, accelerated by the momentum and energy inputs from the magnetosphere, were observed during the ‘B’ and ‘A2’ salvos (15/16 Nov 1980 and 30 Nov/1 Dec resp.), with perturbations as low as 100 km altitude during the ‘B’ salvo. A global model has been used to simulate the wide-scale consequences of these disturbances, and to aid estimation of the integrated energy and momentum inputs.     

A large area multitechnique experiment for hard X-ray astronomy

A balloon-borne multitechnique large area experiment consisting of 2 co-aligned detectors (3200 cm² NaI and 1800 cm² multiwire proportional counters), is described, which is capble of producing observations of the hard X-ray sky with very high sensitivity and good spectral resolution over the whole operative range (15–300 keV).     

“Immiscible alloys” experiment aboard Salyut 7: Results and interpretation of aluminium-indium emulsions solidified in microgravity

The paper describes the main results obtained with the immiscible aluminium-indium alloys elaborated during the Salyut 7 Franco-Soviet space flight. It provides a brief summary of the principle of the experiment, a discussion of the main metallographic and thermal results and, finally, it concentrates on determining the parameters contributing to the formation of the observed structures.     

Aerosol observations from Nimbus-7 CZCS along the South African West Coast

In the course of the South African participation in the Nimbus-7 CZCS project, a fair amount of cloud-free data were collected along the South African West Coast, mainly to study upwelling phenomena. Examples of aerosol radiance maps produced during analysis of these data, including some anomalous results, are discussed.     

An imaging telescope for soft gamma-ray astronomy: The preliminary in-flight tests

A large area (6000 cm²) actively shielded low energy gamma-ray telescope is going to be built by an Anglo-Italian collaboration. The telescope, named ZEBRA, will be capable of producing images of the X and gamma ray sky in the energy range 0.015–20 MeV with an intrinsic angular resolution of a few tenths of a degree. A prototype detector has been built in order to experimentally study the main characteristics of the detection plane. The preliminary results obtained during a balloon flight from Trapani, Sicily in July 1981 are presented.     

The position sensitive low energy detector on board the ZEBRA telescope

In order to improve the low energy capability (15 ÷ 150 KeV) of the balloon borne “ZEBRA” low energy gamma imaging telescope (150 KeV-20 MeV), a large area, high spectral resolution (5% at 60 KeV), low background detector has been designed and is now under development.It consists of two MultiWire Spectroscopic Proportional Counter (SPC), escape gated, that have a sensitive area of 6000 cm², and are placed above the large area array of sodiumiodide position sensitive elements.