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Image:TADRelay1.jpg 200px Thrust Augmented Delta with Relay 1 satellite Category:Launch Vehicle

Image:TATAgenaD.jpg 200px Thrust Augmented Thor with Agena D stage Category:Launch Vehicle

... . High performance military rockets can provide about 3300 feet per second of delta V. Space travel requires a very large delta V. The first objective of a launch to space is to ... second. Landing on the Moon or other planets and returning home requires even more total delta V capability. ---- Answer provided by John W. Cole Image:K2S logosmall.jpg Question and Answer ...

... : Duell, Sloan and Pearce, 271 pages, $4.50'' Documentary history of the development of the Thor intermediate range ballistic missile. Extracted from the 1962 Publication ''Annotated Bibliography of Space Science and ...

... (SI), of the order of 2800 to 5000 s, but with an inherently low thrust and thrust density. However, this latter limitation is due to the restricted power available from present spacecraft. It is shown in this paper that a very much enhanced thrust density can be provided if a nuclear fission power source is utilised, with an electrical ...

... 62 62 '''Page ''' - 15-31 '''Year''' - 2009 '''Keywords''' - Finite elements in time, trajectory optimisation, low-thrust multigravity assist trajectories, direct transcription methods, global optimisation methods '''JBIS Reference Code ''' - 2009.62.15 ... Finite Elements in Time was used for the design and optimisation of the entire low-thrust gravity assist transfer from the Earth to Europa. Prior to that, a global search algorithm ...

Image:ThorAbleStarTransit3A.jpg 200px Thor Able Star with Transit 3A satellite Category:Launch Vehicle

... Interplanetary Society for Volume 61 61 '''Page ''' - 139-145 '''Year''' - 2008 '''Keywords''' - Trajectory optimization, low-thrust, optimal control, non-linear programming, guidance '''JBIS Reference Code ''' - 2008.61.139 '''Number of Pages ... minimum-time transfer between two orbits, including the phasing with a desired spacecraft. Very-low thrust means several hundred revolutions to perform the large change in orbital elements. The optimal control ...

... methods of propulsion systems utilizes the ubiquitous infinite space, more specifically, vacuum. An extraction of thrust from the excited quantum vacuum is indispensable to the development of field propulsion. It is ... yields the coordination geometry of energy density. This paper describes the theoretical possibility of extracting thrust from the excited vacuum induced by controlling squeezed light, and identifies several supporting experimental concepts ...

... , non-dimensional numbers related to performance are beneficial, as they remove effects of scale. Traditionally thrust coefficients and C have been used to quantify the aerodynamic and chemical performance of a system respectively. However, it is argued here that in fact the thrust coefficient does not fully account for aerodynamic performance, as the impact of non-uniform flow ...

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