Developing a Ballistic Software Kit to Estimate Vehicle Characteristics at the Draft Design Stage
<p>The article describes a ballistic software kit to calculate a moving vehicle trajectory in atmosphere and space. Such software gives an opportunity to accelerate the acquisition of flying vehicle’s ballistic parameters at the stage of draft design. It contributes to improving collaboration...
Main Authors: | V. I. Maiorova, D. A. Grishko, V. V. Leonov, E. N. Munin |
---|---|
Format: | Article |
Language: | Russian |
Published: |
MGTU im. N.È. Baumana
2015-01-01
|
Series: | Nauka i Obrazovanie |
Subjects: | |
Online Access: | http://technomag.edu.ru/jour/article/view/359 |
Similar Items
-
Orbit-injection Strategy to a Multistage Launch Vehicle Based on Six-Degree of Freedom and Coupled Axes Attitude Control System
by: Daniel Furlani Aguiar, et al.
Published: (2024-03-01) -
A Six Degrees-of-Freedom Flight Dynamics Simulation Tool of Launch Vehicles
by: Guilherme Silveira, et al.
Published: (2015-05-01) -
Analysis of Propellant Weight under Re-Entry Conditions for a Reusable Launch Vehicle Using Retropropulsion
by: Yongchan Kim, et al.
Published: (2021-05-01) -
Effect of Initial State of Air-launch on Payload of Launch Vehicle
by: CAI Hengyu, et al.
Published: (2020-04-01) -
Performance Analysis on the Small-Scale Reusable Launch Vehicle
by: Zheng Gong, et al.
Published: (2022-09-01)