Historical aspects of human presence in Space

Purpose: This paper presents the development of human presence in Space from its beginnings. Study hypotheses were based on historical findings on scientific, medical, cultural, and political aspects of manned Space flight due to the different attitudes of Space minded nations and organizations. Impacts of aerospace medicine on the advances of biomedical sciences will be touched upon, as well as the historical development of aviation and Space medical achievements which are described briefly and visions for future developments are given.Methods: An overview was gained by literature-study, archives research and oral history taking.Results: Aviation Medicine evolved parallel to Man's ability to fly. War-triggered advancements in aviation brought mankind to the edge of space-equivalent conditions within a few decades of the first motor-flight, which took place in the USA in 1903 [V. Harsch, Aerospace medicine in Germany: from the very beginnings, Aviation and Space Environment Medicine 71 (2000) 447–450 [1]].Forerunners and precursors of aerospace medicine can be found in the fields of high mountain physiology and aviation medicine. In Germany, in 1901, the meteorologists Arthur Berson and Reinhard Suering reached a height of 10,500 m with their balloon “Preussen” in 1901 [V. Harsch, Aerospace medicine in Germany: from the very beginnings, Aviation and Space Environment Medicine 71 (2000) 447–450 [1]]. For further ascents to the stratosphere the aviation-physiologists, Nathan Zuntz (Berlin) and his colleague Hermann von Schroetter (Vienna), in 1905 not only suggested the use of face-fitting breathing-masks, but also the employment of a hermetically sealed cabin [H.C. Gunga, K.A. Kirsch, Nathan Zuntz (1847–1920)—A German pioneer in high altitude physiology and aviation medicine, Aviation and Space Environment Medicine 66 (1995) 168–176 [9]]. Auguste Piccard successfully applied this principle in cooperation with Paul Kipfer in 1931, when they reached a height of 15,781 m [A. Piccard, Über den Wolken, unter den Wellen (Above the clouds, below the waves). Brockhaus, Wiesbaden, 1954 [11]].     

Imaging of local lung ventilation under different gravitational conditions with electrical impedance tomography

The regional lung ventilation depends on the amount and direction of applied gravitational force. This article presents a technique suitable for microgravity condition, providing online information about the local dynamic behavior of the lungs. Using state-differential images measured by electrical impedance tomography (EIT), for every region of interest (ROI) of the lungs a median signal was calculated. For the detection of regional differences in the lung ventilation, local impedance signals were compared with a reference signal, which was the median value over all pixels inside the lungs.We compared both the difference in magnitude and the phase shifts between the ROIs. The phase information was calculated using the Hilbert transform. The technique was tested on five spontaneously breathing subjects.The phase difference proved to be a very sensitive indicator for changes in the regional ventilation during postural changes and therefore changes of the direction of gravitational forces.     

不同燃气环境下硅橡胶绝热材料烧蚀特性试验研究

在气相燃气环境、含Al2O3两相燃气环境中,对硅橡胶绝热材料开展了烧蚀试验研究,分析了不同燃气环境下燃气流速对材料的炭化烧蚀率、炭化层结构特征及炭化层成分分布的影响.试验结果表明,炭化层及热解层膨胀幅度很大,导致的热传导路径增长不可忽略;在烧蚀发动机高温燃气环境中,燃气流速增大对炭化层有明显减薄作用,热解气体溢出受阻对炭化层产生的内压作用以及热应力可能使炭化层结构破坏,炭化层主要成分的摩尔含量沿厚度方向有基本相同的变化趋势;富氧环境中的炭化烧蚀率最大,且烧蚀机理与烧蚀发动机环境有较大区别.     

The effects of prolonged weightlessness and reduced gravity environments on human survival

The manned exploration of the solar system and the surfaces of some of the smaller planets and larger satellites requires that we are able to keep the adverse human physiological response to long term exposure to near zero and greatly reduced gravity environments within acceptable limits consistent with metabolic function. This paper examines the physiological changes associated with microgravity conditions with particular reference to the weightless demineralizatoin of bone (WDB). It is suggested that many of these changes are the result of physical/mechanical processes and are not primarily a medical problem. There are thus two immediately obvious and workable, if relatively costly, solutions to the problem of weightlessness. The provision of a near 1 g field during prolonged space flights, and/or the development of rapid transit spacecraft capable of significant acceleration and short flight times. Although these developments could remove or greatly ameliorate the effects of weightlessness during long-distance space flights there remains a problem relating to the long term colonization of the surfaces of Mars, the Moon, and other small solar system bodies. It is not yet known whether or not there is a critical threshold value of 'g' below which viable human physiological function cannot be sustained. If such a threshold exists permanent colonization may only be possible if the threshold value of 'g' is less than that at the surface of the planet on which we wish to settle.     

Skill maintenance in extended spaceflight: a human factors analysis of space and analogue work environments

This paper discusses the implications of increasing mission lengths of manned spaceflight for the design of future space systems from a human factors point of view. It is argued that the increase in mission duration has brought about a number of new problems, which have not been sufficiently addressed in space research. Therefore, a review of analogue work environments is carried out to make up for the paucity of space research found in the area of human performance in long-duration spaceflight. This resulted in an evaluation of seven analogue environments concerning their similarity to space with industrial process control and nuclear submarines coming out as the closest match on the technical dimension. Finally, some recommendations are given from the lessons learned in spaceflight, simulation studies and appropriate analogue environments.     

Nausogenic properties of various dynamic and static force environments.

Motion sickness can occur when an accelerating force acting on the human body repeatedly changes amplitude and direction or both. It also can occur without any motion after transfer into a constant force field significantly different from Earth-gravity. Dynamic and static causes of motion sickness can be distinguished accordingly. Space sickness, too, has dynamic as well as static aspects. Dynamic space sickness might depend on increased bilateral differential sensitivity of the peripheral and central vestibular apparatus, whereas static space sickness may be caused by erroneous compensation of bilaterial asymmetries of the otolith-system in the microgravity environment. Experiments in airplanes, cars and on a vestibular sled have shown that the susceptibility to motion sickness is highest for changes of acceleration in the negative X-axis (as compared to the other axes) of the body. During reciprocating linear accelerations on the vestibular sled, standstill periods of movement and the direction of movement cannot correctly be indicated, because the peripheral vestibular apparatus lacks true motion detectors.     

Habitability design of European spacecraft Hermes--ergonomic aspects.

First results of a 3-D human body model conception adapted to C.A.D. studies is presented. This parametric model incorporating specific constraints due to weightlessness is well adapted to bring valuable answers to Human Factors Engineers, designing man-system interfaces of European spacecraft Hermes.     

Nonlinear feedback control of low-thrust orbital transfer in a central gravitational field

This paper investigates the problem of continuous-thrust orbital transfer using orbital elements feedback from a nonlinear control standpoint, utilizing concepts of controllability, feedback stabilizability and their interaction. Gauss's variational equations (GVEs) are used to model the state-space dynamics of motion under a central gravitational field. First, the notion of accessibility is reviewed. It is then shown that the GVEs are globally accessible. Based on the accessibility result, a nonlinear feedback controller is derived which asymptotically steers a spacecraft form an initial elliptic orbit to any given elliptic orbit. The performance of the new controller is illustrated by simulating an orbital transfer between two geosynchronous Earth orbits. It is shown that the low-thrust controller requires less fuel than an impulsive maneuver for the same transfer time. Closed-form, analytic expressions for the new orbital transfer controller are given. Finally, it is proven, based on a topological nonlinear stabilizability test, that there does not exist a continuous closed-loop controller that can transfer a spacecraft onto a parabolic escape trajectory.     

Satellite dynamics under the influence of gravitational and aerodynamic torques. A study of stability of equilibrium positions

The dynamics of the rotational motion of a satellite, moving in the central Newtonian force field under the influence of gravitational and aerodynamic torques, is investigated. The paper proposes a method for determining all equilibrium positions (equilibrium orientations) of a satellite in the orbital coordinate system for specified values of aerodynamic torque and the major central moments of inertia; the sufficient conditions for their existence are obtained. For each equilibrium orientation the sufficient stability conditions are obtained using the generalized energy integral as the Lyapunov function. The detailed numerical analysis of the regions where the stability conditions of the equilibrium positions are satisfied is carried out depending on four dimensionless parameters of the problem. It is shown that, in the general case, the number of satellite’s equilibrium positions, for which the sufficient stability conditions are satisfied, varies from 4 to 2 with an increase in the value of the aerodynamic torque magnitude.     

Eddy currents induced migration of droplets in electrically conducting fluid in microgravity environments

Electrical eddy currents induced migration of droplets, whose conductivity differs from that of surrounding fluid, is analysed. Eddy currents in a dilute suspension under consideration, which fills the dielectric tube, are induced by alternating magnetic field parallel to the tube axis. In the case where the droplet radius is small as compared to the skin depth, the distributions of magnetic fields, currents and electromagnetic forces inside and outside the droplet have been calculated. For small Reynolds numbers, with neglecting inertial and thermocapillary effects and the gravity, the flow of fluids around the droplet and inside it, caused by electromagnetic forces, has been studied. The formula is obtained, which relates the droplet migration velocity to the electro-magnetic field, the droplet size and physical properties of fluids.     

Reflections on human presence in space.

Humankind's exploration of Space has until now been understood as analogous to that of planet Earth: sending out crews to far-off, unknown lands in the hope of finding supplies of food, water or energy along with shelter and living-space. But Space is turning out to be much less hospitable than our earthly milieu in terms of resources as well as energy costs. It seems appropriate to ask what level of adaptation is needed for humans to travel and live in the cosmos, and to assess if the next logical step should necessarily be a programme of conquest analogous to that of the Moon--for example, towards Mars. Should we not rather be making more use of Earth's immediate neighbourhood, namely the sphere of a million of kilometres we call "Greater Earth"? In the same way, it is appropriate to ask questions about the conception of human beings which will from now on sustain the conquest of Space. The astronaut of the last forty years is the direct heir of the explorers of Ancient and Modern times; now, through the influence of science and technology, humanity has been put "into motion" not only geographically, but also in its most essential foundations: culture, psychology, philosophy. If the development of telepresence technology now gives us the ability to talk about a "Greater Human Being", it is chiefly through freedom of choice for oneself, for humanity and even for Earth.     

Chemical aspects in shock ignition of fuel drops

The behavior, in an oxygen atmosphere, of shocked drops of nitromethane, 1- and 2- nitropropane, ethyl and propyl nitrate, decane, and heptane was studied. Results suggest a new mode of ignition for nitrates at high incident shock Mach numbers (M 3.7). At the high incident shock strengths ignition occurs in the boundary layer, but no blast wave develops as is the case for lower shock strengths. Since ignition delay times are very short under these conditions, the absence of blast waves is attributed to the lack of time for the accumulation of fuel in the wake. Gas phase studies of the shock decomposition of fuel molecules were undertaken to determine if gas phase data could be used to explain the trends in the drop ignition observations. Nitromethane and the nitrates were mainly used in this effort. Alternative explanations for the role of gas phase kinetics in the ignition of drops are presented.     

Some aspects of continuous flow electrophoresis in microgravity

Zone electrophoresis is a highly efficient method of separating biological products. It is based on the differences of mobilities of ionized particles in an electric field. During the separation complications arise due to electro-osmosis or thermal convection generated by Joule heating.This paper analyses the hydrodynamical running of a continuous flow zone electrophoresis cell and shows the influence of specific parameters on the separation.The modelling of the flow structure of the buffer solution is developed. The equations and the corresponding boundary conditions are solved by finite difference method. The model established provides knowledge of the hydrodynamical perturbations generated by electro-osmosis and thermal free convection. The case of microgravity is considered.     

The future of human spaceflight.

After the Apollo Moon program, the international space station represents a further milestone of humankind in space, International follow-on programs like a manned return to the Moon and a first manned Mars Mission can be considered as the next logical step. More and more attention is also paid to the topic of future space tourism in Earth orbit, which is currently under investigation in the USA, Japan and Europe due to its multibillion dollar market potential and high acceptance in society. The wide variety of experience, gained within the space station program, should be used in order to achieve time and cost savings for future manned programs. Different strategies and roadmaps are investigated for space tourism and human missions to the Moon and Mars, based on a comprehensive systems analysis approach. By using DLR's software tool FAST (Fast Assessment of Space Technologies), different scenarios will be defined, optimised and finally evaluated with respect to mission architecture, required technologies, total costs and program duration. This includes trajectory analysis, spacecraft design on subsystem level, operations and life cycle cost analysis. For space tourism, an expected evolutionary roadmap will be described which is initiated by short suborbital tourism and ends with visionary designs like the Space Hotel Berlin and the Space Hotel Europe concept. Furthermore the potential space tourism market, its economic meaning as well as the expected range of the costs of a space ticket (e.g. $50,000 for a suborbital flight) will be analysed and quantified. For human missions to the Moon and Mars, an international 20 year program for the first decades of the next millennium is proposed, which requires about $2.5 Billion per year for a manned return to the Moon program and about $2.6 Billion per year for the first 3 manned Mars missions. This is about the annual budget, which is currently spend by the USA only for the operations of its Space Shuttle fleet which generally proofs the affordability of such ambitious programs after the build-up of the International Space Station, when corresponding budget might become again available.     

Numerical solutions to exact equations of motion along near-optimal multi-orbit trajectories for a spacecraft in a Newtonian gravitational field

The actual topic of optimization of multi-orbit low-thrust spacecraft inter-orbital transfers is considered. We have developed an original approach to solving this problem, and it is described.     

Simulation of human reactions under extreme conditions.

Lung mass determination in cooperative subjects is possible by computation from the "flow-volume" loop, if total lung resistance (Raw) is known. The model is applicable to tracking changes in weightlessness. Modifications for improving the result are discussed.     

The use of micro-worlds for human factors research in extended spaceflight.

This article provides an analysis of the utility of micro-worlds for human factors research in extended spaceflight. It outlines potential areas of application of the micro-world research paradigm in the context of spaceflight. While the research literature provides several examples of micro-worlds that simulate different work environments of high complexity, little work has been done with this tool in the operational environment of spaceflight. The author presents a micro-world, called CAMS, that has been especially developed for use in space-related research. The results from a research programme (comprising seven studies using CAMS) are presented. Based on a comparative analysis of the benefits and limitations of micro-worlds compared to other simulation types, the author argues that micro-worlds can be a very effective tool, provided their inherent limitations are taken into consideration.     

Oxygen regimen in the human peripheral tissue during space flights.

A survey of the results of the experiment "Oxygen," carried out within the scope of the INTER-KOSMOS program in members of the permanent crews and of international visiting expeditions to the Soviet orbital station Salyut-6, is given. During the 7-day space flights of the international visiting expeditions a significant decrease in pO2ic by 3.28 kPa was observed. Local oxygen utilization reduced significantly by 0.44 kPa. During hyperventilation testing after return to earth a statistically significant decrease in the peak value by 1.39 kPa was noted. In the long-term crews of the orbital station Salyut-6 the highest decrease in pO2ic of 3.8 kPa and the absolutely lowest value of 3.4 -/+ 0.5 kPa during space flight were observed. The decrease in local oxygen utilization during the flight of 0.8 kPa/min was greater than that of the visiting crews. The results indicate the importance of investigating the dynamics of the oxygen regimen for medical control of the crew members both during the space flight and during the readaptation phase after return to earth.