scholarly journals Energetic Compositions Application for the Reduction of the Environmental Pollution Because of Space Vehicle Launches

2017 ◽  
Vol 19 (3) ◽  
pp. 239 ◽  
Author(s):  
V. Trushlyakov ◽  
D. Lempert ◽  
Yuan-Jie Shu

Technogeneous impact of rocket and space activities on the environment is one of the most actual problems of practical cosmonautics. This technogeneous impact is not only the pollution of near Earth space with space debris (worked-off stages of space launch vehicle (SLV)), but also the pollution of significant areas on the Earth surface with worked-off lower stages of SLV, which fall down after having accomplished their mission. In OmSTU and IPCP RAS it was suggested to apply different self-burning compositions, generating hot gases for the evaporation of the unused residues of liquid propellant in tanks of SLV. Then the mixture of the evaporated compounds together with the gaseous combustion products from gas-generating compositions is used as propellant mixture for the autonomous gas rocket engine. Such a solution would decrease considerably the level of the environment pollution and additionally it increases the energetic characteristics of SLV. For example, in the case of the second stage of SLV «Soyuz-2.1.v» it increases the total velocity by 5%. Also it is proposed to use firing the pyrotechnic compositions like (thermites) for the fairings heating up to the temperature when the fairing material can be ignited in air. It would reduce considerably the amount and the mass of the separating parts of SLV that fall to the Earth.

2017 ◽  
Vol 19 (1) ◽  
pp. 63
Author(s):  
V. Trushlyakov ◽  
K. Zharikov ◽  
D. Lempert

The choice is discussed of solid gas generating compositions for venting by hot combustion products a fuel tank of the spent orbital stage of a space launch vehicle with a main liquid rocket engine. Non explosiveness is achieved via eliminating the<br />possibility of freezing the drainage system when products of gasification (vapours of a propellant component + the remains of a gas boost + the hot products of combustion of solid gas generating compositions) are discharged from the tank into surrounding space. There are imposed requirements, constraints, and criteria for selecting solid gas generating compositions. When considering tank with the residues of liquid oxygen belonging to orbital spent stage of the launch vehicle «Zenith» the ways are shown how to ensure explosion safety, which on the basis of proposed approaches by selecting solid gas generating compositions (SGC) which generate oxygen and<br />nitrogen. As a criterion of choice of SGC the total mass of the gasification system is adopted, which includes the SGC mass for gasification of liquid propellant residues, the mass of the gas generator and the mass of system to supply the combustion products of SGC into the tank. It is proposed use of residual heat in the condensed phase of the SGC combustion products to heat up the drainage system, which will increase the probability of a trouble-free operation of the drainage system.


2018 ◽  
Vol 172 ◽  
pp. 01007
Author(s):  
Harish Panjagala ◽  
E L N Rohit Madhukar ◽  
I Ravi Kiran

Due to increasing demand of High Speed Re-entry vehicles for Space activities within the world, a serious issue associated with the method of deceleration down a vehicle is by the intense heat generated because of development of stronger shocks at the nose. The price of thermal protection systems (TPS) to cut back the warmth generated by the return vehicles is extremely high. In this paper, the ultimate outcome is to cut back the aero heating which is achieved by introducing a spike at frontal region of the nose. Additionally, this spike avoids the deterioration and preserves the structural integrity of space vehicle over elevated temperatures. Further, four totally different geometries of tip specifically Blunt, Slender, Snap and Pan for the aerospike has been introduced and their impact on performance is evaluated and compared with the vehicle having TPS. Hence, usage of aerospike in return vehicles is the most successful and economical over different protection system.


1990 ◽  
Vol 123 ◽  
pp. 347-354
Author(s):  
G. A. Keyworth

None of us thought, when this colloquium was scheduled, that the timing would enable it to become a celebration as well. The launch, after years of postponements, of the Hubble Space Telescope, has cast a galactic glow over the proceedings here this week. But at the same time, the frustrating delays caused by the collapse in 1986 and very slow regeneration of the U.S. space launch capabilities since then make this discussion of near-earth access very pointed.As we know, the sheer momentum of the U.S. Space Shuttle Program has dominated our perceptions of space launch for a decade and a half. It reached its peak in the early 1980s when our national policy placed nearly total reliance on the Shuttle as our means of access to space. It was a policy doomed to fail, for obvious and not-so-obvious reasons.


1997 ◽  
Vol 165 ◽  
pp. 71-78
Author(s):  
Edwin Wnuk

AbstractTwo aspects of the orbital evolution of space debris – the long-term evolution and the short-term one – are of interest for an exploration of the near- Earth space. The paper presents some results concerning the estimation of the accuracy of predicted positions of Earth-orbiting objects for the short-term: a few revolutions or a time-span interval of a few days. Calculations of predicted positions take into account the influence of an arbitrary number of spherical coefficients of the Earth gravity potential. Differences in predicted positions due to differences in the best contemporary geopotential models (JGM-2, JGM-3 and GRIM4-S4) are estimated with the use of an analytical theory of motion and a numerical integration.


Author(s):  
Martha Mejía-Kaiser

International space law is a branch of public international law. Norms of treaty law and customary law provide a foundation for the behavior of the subjects of international law performing space activities. Five multilateral space treaties are in effect, which are complemented by important recommendations of international organizations such as United Nations (UN) General Assembly Resolutions and International Telecommunication Union (ITU) Regulations. The Inter-Agency Space Debris Mitigation Coordination Committee (IADC), a non-governmental body composed of several space agencies (for instance, the European Space Agency, the United States National Aeronautics and Space Administration, the Japanese Aerospace Exploration Agency, the Russian Federal Space Agency), issued its Space Debris Mitigation Guidelines in 2002. The IADC defines “space debris” as “all man-made space objects including fragments and elements thereof, in Earth orbit or re-entering the atmosphere, that are non-functional” (IADC, 2002, Revision 1, 2007, 3.1. Space Debris). Although the term “space debris” was not included in any space treaty, the drafters of the space treaties considered space objects as “hazardous” because “component parts of a space object as well as its launch vehicles and parts thereof” detach in course of normal launching operations, because space objects can fragment during an attempted launch, and because space objects that re-enter Earth’s atmosphere and survive friction have the potential to cause damage. In addition, radioactive and chemical substances on board space objects may represent a hazard to populations and the environment on the Earth. Besides the threats to aircraft in flight and to persons and property on the surface of the Earth, space debris in orbit is increasing alarmingly and poses a threat to manned space missions and non-manned space objects. While the Convention on International Liability for Damages Caused by Space Objects (Liability Convention, 1972) considers the threats of space objects during launch, in outer space, and when entering the Earth’s atmosphere, there have been efforts to minimize the generation of space debris in orbit, outside the framework of the space treaties. The IADC Space Debris Mitigation Guidelines are a comprehensive list of recommendations to launching states, owners, and operators of space objects. They are increasingly recognized by states through the creation of codes of conduct, national legislation, recommendations of international organizations, and state practice. Furthermore, non-governmental institutions, like the International Organization for Standardization, are providing more detailed technical instructions for the implementation of the Space Debris Mitigation Guidelines, which are a breakthrough for the application of the guidelines by states of different economic and technical standing. Even though states are reluctant to accept new obligations through treaties, recommendations and state practice are becoming powerful instruments to avert the dangers of hazardous space debris that may create damage on the Earth or in orbit. Space debris also is becoming one of the drivers for the initiatives of the United Nations on the long-term sustainability of outer space activities to promote the existing mitigation guidelines and to formulate new guidelines for clearing outer space of debris.


2018 ◽  
Vol 55 (2) ◽  
pp. 382-402
Author(s):  
Manish Mehta ◽  
C. Mark Seaford ◽  
Robert D. Kirchner ◽  
Aaron T. Dufrene

2013 ◽  
Vol 2013 ◽  
pp. 1-12 ◽  
Author(s):  
Denilson Paulo Souza dos Santos ◽  
Antônio Fernando Bertachini de Almeida Prado ◽  
Evandro Marconi Rocco

The Multiple Encounters Problem is described in the literature as the problem of finding trajectories for a spacecraft that leaves from a mother planet, describes a trajectory in the interplanetary space, and then goes back to the mother planet. The present paper extends the literature and the departure and arrival angles of the spacecraft are generalized to be nonsymmetrical. The solutions are shown in terms of the true (ν) and eccentric anomaly (η). The velocity variation (Δ V) required for the transfer is also shown. Then, this study is generalized to consider the possibility that the spacecraft makes a close approach with the mother planet to change its energy in the return trip. The velocity (Δ V) and energy variation (Δ E) due to this passage are obtained. The topics studied here can be applied in missions that leave and come back to the Earth, with the goal of studying the interplanetary space, as well as for missions whose objective is to make an alteration in the energy of the space vehicle through a swing-by with the mother body.


Author(s):  
I. B. Kolyado ◽  
S. V. Plugin ◽  
S. I. Tribunsky ◽  
A. A. Karpenko

Introduction. On the territory of the Altai territory there are four areas of falling of separating parts of space launch vehicles. For many years, these territories have been exposed to negative factors of rocket and space activities. In order to assess the possible impact of rocket and space activities on the health of the inhabitants of the Altai territory, living near the areas of falling of the separating parts of the launch vehicles, their medical examination is regularly carried out.The aim of the study is to assess the possible impact of rocket and space activities on public health.Materials and methods. Th e results of dynamic analysis of the prevalence of circulatory disease among the residents of Novoaleysky and Ploskovsky village councils of the Tretyakov District of the Altai territory. In 1999, 1929 people were examined, in 2005–1213 people, in 2010–1016 people and in 2015–843 people. Extensive and intensive indicators of prevalence of diseases of the circulatory system were obtained.Results. Basing to results of the dynamic analysis, the peculiarities of the signifi cance and prevalence of the circulatory system diseases, as well as of separate nosologies of this class, were identifi ed. Th e most common circulatory system diseases were determined for the studied contingent. Th e prevalence of this pathology diff ers in men and women. Comparison of the results of the medical examination in 2015 with the data on the general morbidity of the population of the Altai territory showed that the level of detection of diseases of the circulatory system among the inhabitants of the studied areas is signifi cantly higher than the level of the general morbidity of this pathology. Th e obtained results of the analysis of the prevalence of the circulatory system diseases allow overtime monitoring the residents’ health of the territories boarding to the areas of rocket and space activities. Th is allows to evaluate the eff ectiveness of measures to optimize their health and provides sound information for management decisions.Conclusions. Th e overall prevalence of diseases in the study areas in 2015 was signifi cantly lower than in 1999, but the prevalence of diseases of the circulatory system in 2015 was signifi cantly higher than in 1999. In the study areas, the most signifi cant diseases of the circulatory system are hypertension, myocardiodystrophy, angina pectoris and atherosclerosis of the aorta. In all the years studied, the prevalence of circulatory diseases among women was signifi cantly higher than among men. Among women, the prevalence of myocardiodystrophy of various etiologies and hypertension is signifi cantly higher. Th e prevalence of angina in men and women was the same. Th e prevalence of aortic atherosclerosis is much higher in men.


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