Meteors do not break exogenous organic molecules into high yields of diatomics

Meteoroids that dominate the Earth's extraterrestrial mass influx (50-300 microm size range) may have contributed a unique blend of exogenous organic molecules at the time of the origin of life. Such meteoroids are so large that most of their mass is ablated in the Earth's atmosphere. In the process, organic molecules are decomposed and chemically altered to molecules differently from those delivered to the Earth's surface by smaller (<50 microm) micrometeorites and larger (>10 cm) meteorites. The question addressed here is whether the organic matter in these meteoroids is fully decomposed into atoms or diatomic compounds during ablation. If not, then the ablation products made available for prebiotic organic chemistry, and perhaps early biology, might have retained some memory of their astrophysical nature. To test this hypothesis we searched for CN emission in meteor spectra in an airborne experiment during the 2001 Leonid meteor storm. We found that the meteor's light-emitting air plasma, which included products of meteor ablation, contained less than 1 CN molecule for every 30 meteoric iron atoms. This contrasts sharply with the nitrogen/iron ratio of 1:1.2 in the solid matter of comet 1P/Halley. Unless the nitrogen content or the abundance of complex organic matter in the Leonid parent body, comet 55P/Tempel-Tuttle, differs from that in comet 1P/Halley, it appears that very little of that organic nitrogen decomposes into CN molecules during meteor ablation in the rarefied flow conditions that characterize the atmospheric entry of meteoroids approximately 50 microm-10 cm in size. We propose that the organics of such meteoroids survive instead as larger compounds.     

Proton Events and X-ray Flares in the Last Three Solar Cycles

A database joining the available information about proton enhancements near the Earth and their possible solar sources is organized on the basis of proton measurements of the GOES and IMP-8 satellites, the data of neutron monitors, and GOES X-ray measurements. One thousand one hundred and forty-four proton events with energy > 10 MeV have been selected in the period from 1975 to 2003. More than a half of these events can be reliably related to X-ray solar flares. A statistical analysis shows the probability of observing solar protons near the Earth and their maximum flux value to be strongly dependent on the importance of a flare and its heliolongitude. Proton events are recorded after all suitably located (western) flares with X-ray importance > X5. The heliolongitude of a flare predetermines the character of the time profile of proton events in many respects. The relationship of proton events with the other characteristics of flares is established. The flares associated with proton enhancements are characterized by longer duration, slower rise to the X-ray maximum, smaller temperature, and larger length of the X-ray loops.__________Translated from Kosmicheskie Issledovaniya, Vol. 43, No. 3, 2005, pp. 171–185.Original Russian Text Copyright © 2005 by Belov, Garcia, Kurt, Mavromichalaki.     

Electronics brain design for advanced microspacecraft

A brief history of NASA robotic spacecraft computing architectures is given. Changing needs driving changes in features (10x reduction in cost, various increases in capability, 10x to 100x reduction in power, mass and volume) for spacecraft computing are discussed. An architecture which addresses these changes is proposed. Finally, future directions of exploration for this spacecraft computing architecture are considered.     

Ethical problems of interaction between ground-based personnel and orbital station crewmembers.

Manned missions onboard orbital stations Salyut-6 and Salyut-7 have led us to the conclusion that a long-term space mission can be viewed as a complex socio-man-machine system whose effectiveness largely depends on the quality of interaction between its subsystems. When analyzing and assessing the reliability of this system, it is important to consider ethical aspects, because they concern human relations, permeating its very component and in the long run determining its efficiency. Psychological and medical examinations before, during and after manned missions have helped us to identify the major points of interaction of the subsystems which require adequate monitoring and optimization using socio-psychological and organization-technical approaches: arrangement and evaluation of the quality of work, arrangement of proper leisure, psychological comfort in the interpersonality and intergroup relations during prolonged space missions. This paper also discusses adaptive changes in the mental and physical state due to prolonged exposure to space flight factors such as microgravity and confinement.     

The real aerospace plane

In this article reproduced from Aerospace, Spring 1986, James Haggerty reports on the US National Aerospace Plane (NASP) research programme. NASP is a joint Department of Defense/NASA programme to develop and demonstrate the technologies for a revolutionary class of aerospace vehicles, powered by airbreathing engines, that would have the capability to take off from and land horizontally on standard runways, cruise in the atmosphere at hypersonic speeds, or fly into low-Earth orbit. The Air Force has been named executive agency for the programme. NASA is charged with overall technology direction. Other DoD participants include DARPA, the Navy and the Strategic Defense Initiative Organization.

In April 1986, the USAF awarded development contracts to seven aerospace manufacturing firms. Contracts for air-frame design went to Boeing Aerospace Company, Lockheed Advanced Aeronautics Company, General Dynamics Corporation, McDonnell Douglas Corporation and Rockwell International Corporation. General Electric Company and Pratt & Whitney Division of United Technologies were awarded propulsion contracts.     

Pathophysiology of motor functions in prolonged manned space flights.

The influence of weightlessness on different parts of the motor system have been studied in crew members of 140 and 175 days space flights. It has been shown that weightlessness affects all parts of the motor system including (i) the leg and trunk muscles, in which severe atonia, a decrease of strength and an increase of electromyographic cost of contraction have been observed, (ii) the proprioceptive elements and the spinal reflex mechanisms in which decreased thresholds accompanied by decreases of maximal amplitude of reflexes and disturbances in cross reflex mechanisms have been found. and (iii) the central mechanisms that control characteristics of postural and locomotor activities. The intensities and durations of disturbances of different parts of the motor system did not correlate to each other, but did correlate with prophylactic activity during space flight. The data suggest a different nature of disturbances caused by weightlessness in different parts of the motor system.     

Summary of medical investigations in the U.S.S.R. manned space missions.

The results of biomedical investigations carried out in the U.S.S.R. manned space missions are discussed. Their basic result is well-documented evidence that man can perform space flights of long duration. The investigations have demonstrated no direct correlation between inflight or postflight physiological reactions of crewmembers and flight duration. In all likelihood, this can be attributed to the fact that special exercises done inflight efficiently prevented adverse effects of weightlessness. However, human reactions to weightlessness need further study. They include negative calcium balance and anemia as well as vestibulo-autonomic disorders shown by crewmembers at early stages of weightlessness. Attention should be given to psychological, social-psychological and ethical problems that may also limit further increase in flight duration.     

Stability of dynamic algorithms of determination of quasi-stationary satellite orbits

A method of estimating the stability of the problem of orbit determination under disturbances caused by finite accuracy of calculation and geographical siting of observation stations is proposed.     

Space transportation system: Upper stage possibilities

This study is concerned with STS upper stages; in particular, the question of reusability vs expendability is addressed.The main result is: reusability seems to be of economic advantage in the lower performance requirement field, and expendability seems to be the more attractive in the case of high performance requirement. The boundary between “low” and “high” performance requirement can be well defined, and is of course dependent upon the technology applied.Whereas single-stage conventional chemical rocket upper stages compatible with STS are the main focal point of this study, several less conventional possibilities are identified. So a second major result is, that in spite of many years of study by competent authors the field is not yet fully understood.Finally: Study method and some of the results are applicable to the more general question of optimum OTV design.     

Some technical aspects of gaseous detonation

This paper briefly describes two attempts to utilize detonative combustion processes to MHD conversion of thermal energy of fuel to electrical energy and bonding of atmospheric nitrogen. For this purpose a continuous impulse detonation chamber with a frequency up to 200 cps was constructed. Using methane-oxygen-nitrogen mixtures the chamber was maintained in stable operation for several hundred hours. Oil was also employed as fuel.Estimates based on experimental data showed that up to 2% of chemical energy of the fuel may be converted into electrical energy. The use of an accelerating nozzle may improve this result.The concentration of nitrogen oxide in combustion products of the detonation wave was higher by 14% than that expected under usual combustion conditions.The advantages of this type of apparatus are: absence of compressors for fuel and oxidant, impulse current generation, low temperatures of chamber walls, and operation over a large range of operating conditions.Problems associated with the effect of the magnetic field on the propagation of the detonation wave are discussed and the possibility of applying the Zeldovich theory to the case of MHD interaction is described. It is shown that the detonation velocity may either increase or decrease depending on the relative orientation of the direction of magnetic field with respect to the detonation wave.