Launcher modeling
Space Trajectories. Launch on Orbit
Quizzed article REF: TRP4059 V1
Launcher modeling
Space Trajectories. Launch on Orbit

Author : Max CERF

Publication date: March 10, 2021, Review date: September 21, 2021 | Lire en français

Logo Techniques de l'Ingenieur You do not have access to this resource.
Request your free trial access! Free trial

Already subscribed?

1. Launcher modeling

The launcher is considered as an undeformable solid of variable mass subjected to internal and external pressure forces. This section presents force models, equations of motion and staging design.

1.1 Force models

SCROLL TO TOP

1.1.1 Pressure forces

Rocket propulsion uses the reaction principle. Propellants are mixed and burned in the combustion chamber. Under the effect of pressure, the gases are expelled towards the nozzle. The convergent-divergent nozzle accelerates the gases to transonic velocity...

You do not have access to this resource.
Logo Techniques de l'Ingenieur

Exclusive to subscribers. 97% yet to be discovered!

You do not have access to this resource. Click here to request your free trial access!

Already subscribed?


Article included in this offer

"Aerospace systems"

( 77 articles )

Complete knowledge base

Updated and enriched with articles validated by our scientific committees

Services

A set of exclusive tools to complement the resources

View offer details