Min Wei
Abstract
In this paper from analysis for the expressions of characteristic velocity for-rocket,it point out the affinity for the question of maximum payload and the best propellant plan.Thus it solves the questions of maximum payload.
A significance statement is not available in the OpenAlex record.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
In this paper from analysis for the expressions of characteristic velocity for-rocket,it point out the affinity for the question of maximum payload and the best propellant plan.Thus it solves the questions of maximum payload.
Key concepts: Payload (computing), Rocket (weapon), Aerospace engineering, Propellant, Point (geometry), Aeronautics, Plan (archaeology), Engineering