Sentence examples for minimum fuel solution from inspiring English sources

Understanding that the minimum fuel solution lies with a semi-major axis ratio of 1, a very accurate empirical approximation is presented for semi-major axis ratio values less than and greater than 1.

Results from this model are shown to provide a reduction in propellant mass required over previous minimum fuel solutions.

Numerical results show that the minimum-fuel solution for the terminal tangent burn rendezvous is close to that for the cotangent rendezvous when the rendezvous time is long enough; however, the cotangent rendezvous may not exist when the rendezvous time is short.

It is shown how the reduction of the minimum loading solution from a two- to a one-group model retains the flat flux in the core but fails to satisfy the thermal boundary condition unless a reflector, with the flux-trap, is used so that without it, the two-group minimum fuel loading solution cannot fully transform to a minimum loading in one group.

In order to determine under what conditions the combination of a floor-heating-based greenhouse with a waste-to-energy plant can be profitable, a mixed integer optimisation model is introduced to allow selection of the minimum cost fuel solution as a function of different design variables of the greenhouse, such as indoor temperature settings and floor area.

In this study, a maximum and a minimum conversion efficiency of fuel solution was obtained as 99 and 98 % from applying 3 and 4 M HCl solutions, respectively.

Considering the minimization of time, the solution cannot be the solution of minimum fuel consumption, because the minimization of time and the minimization of fuel are conflicting objectives.

It was observed at 3 M HCl that a maximum of 660 ml/min and a minimum of 267 ml/min H2 stream rate were obtained from 25 and 10 wt% NaBH4, respectively, from applying a fuel solution rate of 0.97 ml/min.

American intelligence officials long argued that disclosing the numbers would help terrorists calculate the minimum fuel needed for a weapon.

The solution to a transfer which minimizes the square of the thrust magnitude is used as a preliminary guess for the minimum fuel problem, thus allowing for faster convergence to a wider range of problems.

The paper addresses the multiobjective optimization model for achieving the maximum throughput at minimum fuel consumption.