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Equations first rocket equation

Rocket propulsion moves a vehicle by ejecting mass out of the backside of the vehicle. Since there is no atmosphere in space, all of the reaction (i.e. propellant) mass must be carried on board and is usually released as a heated gas (i.e. the exhaust) expanding through a nozzle. All launches from earth into space have used chemical propulsion systems (i.e. reactions between a fuel and an oxidizer). The performance of a rocket vehicle is represented by the so-called first rocket equation ... [Pg.382]

Aspiration rate is only a small part of the overall transport process in flame spectrometry. The production of aerosol and its transport through the spray chamber are also of great importance. The size distribution of aerosol produced depends upon the surface tension, density, and viscosity of the sample solution. An empirical equation relating aerosol size distribution to these parameters and to nebulizer gas and solution flow rates was first worked out by Nukiyama and Tanasawa,5 who were interested in the size distributions in fuel sprays for rocket motors. Their equation has been extensively exploited in analytical flame spectrometry.2,6-7 Careful matrix matching is therefore essential not only for matching aspiration rates of samples and standards, but also for matching the size distributions of their respective aerosols. Samples and standards with identical size distributions will be transported to the flame with identical efficiencies, a key requirement in analytical flame spectrometry. [Pg.32]

In this chapter, the equation governing the statistical counting procedure for sprays is first derived (Section 11.1) and is applied (Section 11.2) to a very simplified model of rocket-chamber combustion in order to obtain an estimate of the combustion efficiency. This illustrative example and others... [Pg.447]

Using Numbers The space shuttle gains nearly 72% of its lift from its solid rocket boosters (SRBs) during the first two minutes of launch. The two pencil-shaped SRB tanks are attached to both sides of the liquid hydrogen and oxygen fuel tank. Each SRB contains 495 000 kg of an explosive mixture of ammonium perchlorate and aluminum. The unbalanced equation for the reaction is given below. [Pg.647]

The reactions of NH3 and CI2 (diluted with N2) or aqueous NaOCl (the first step in reaction 15.33) yield chloramine, 15.16, the compound responsible for the odour of water containing nitrogenous matter that has been sterilized with CI2. Chloramine is unstable, and violently explosive, and is usually handled in dilute solutions (e.g. in H2O or Et20). Its reaction with Me2NH (equation 15.41) yields the rocket fuel 1,1-dimethylhydrazine. [Pg.448]

Sputnik 1, launched on October 4, 1957, by the Soviet Union, was the first artificial satellite. It used radio transmission to collect data regarding the distribution of radio signals within the ionosphere in order to measure density in the atmosphere. In addition to space satellites, the most common artificial satellites are the satellites used for communication, weather, navigation, and research. These artificial satellites travel around the Earth because of human action, and they depend on computer systems to function. A rocket is used to launch these artificial satellites so that they will have enough speed to be accelerated into the most common types of circular orbits, which require speeds of about 27,000 kilometers per hour. Some satellites, especially those that are to be used at locations far removed from the Earth s equator, require elliptical-shaped orbits instead, and their acceleration speeds are 30,000 kilometers per hour. If a launching rocket applies too much energy... [Pg.380]


See other pages where Equations first rocket equation is mentioned: [Pg.28]    [Pg.28]    [Pg.106]    [Pg.34]    [Pg.244]    [Pg.64]    [Pg.100]    [Pg.327]    [Pg.448]    [Pg.100]    [Pg.327]    [Pg.448]    [Pg.790]    [Pg.476]    [Pg.289]    [Pg.253]   
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