Evaluation of Multistage Space and Missile Systems Using the Analysis of the Launch Mass Sensitivity to Design Changes
Author:
- 1 June 2024
- journal article
- Published by Allerton Press in Russian Aeronautics (Iz VUZ)
- Vol. 67 (2) , 340-351
Abstract
The paper continues the theme developed by the author of the application of sensitivity analysis of the initial mass of aircraft to design changes. In thisKeywords
This publication has 4 references indexed in Scilit:
- Conceptual assessment of the fuel efficiency of passenger aircraft with the transition to composite wingsCivil Aviation High Technologies, 2023
- Evaluation of the Mass and Aerodynamic Efficiency of a High Aspect Ratio Wing for Prospective Passenger AircraftAerospace, 2022
- Conceptual Assessment of the Possibility of Using Cryogenic Fuel on Unmanned Aerial VehiclesDrones, 2022
- Analysis of the influence of the scheme of flight of the stage with a reactive recovry system on the energy characteristics of a two-stage medium class launch vehicleVESTNIK of Samara University. Aerospace and Mechanical Engineering, 2016