Analytical Shaping of a Rocket Nose as a Stage of Preliminary Aerodynamic Modification
The article discusses the problem of a preliminary analytical method for modifying the shape of a rocket’s nose. The purpose of this method is to determine the shape that minimizes aerodynamic drag, in the context of modifying a ballistic missile to incorporate guidance systems. The traditional desi...
Saved in:
| Main Authors: | Adrian Szklarski, Robert Głębocki |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2025-06-01
|
| Series: | Aerospace |
| Subjects: | |
| Online Access: | https://www.mdpi.com/2226-4310/12/7/594 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Evolution of Multiple Launch Rocket Systems from Early Rockets to HIMARS and Beyond
by: Mykola Bondarenko, et al.
Published: (2024-11-01) -
DETERMINATION OF ANTIAIRCRAFT GUIDED ROCKETS SUPPLY OF NOT FULLY ACCESSIBLE GROUPING OF ANTIAIRCRAFT ROCKET TROOPS FOR PROVIDING EFFECTIVE REPULSE OF AN AIR ENEMY
by: Spartak Y. Hohoniants
Published: (2014-12-01) -
Influence of Mass Parameters Modification on Manoeuvrability of 9K33 „OSA” Set 9M33M3 Missile
by: Maciej K. CICHOCKI, et al.
Published: (2020-09-01) -
Research on Foreign Air-to-Ground Missiles Development in 2023
by: Liu Ying, Shen Xin, Ren Chunyan
Published: (2024-10-01) -
MODELING THE FLIGHT TRAJECTORY OF OPERATIONAL-TACTICAL BALLISTIC MISSILES
by: I. V. Filipchenko, et al.
Published: (2018-03-01)