Flight Mechanics and Control Problems of Two-Stage-to-Orbit Vehicles: Wind Tunnel Tests for Modelling the Separation Dynamics of a Two-Stage-to-Orbit Vehicle

Christian Zähringer; Gottfried Sachs

doi:10.1002/3527605711.ch6

Flight Mechanics and Control Problems of Two-Stage-to-Orbit Vehicles: Wind Tunnel Tests for Modelling the Separation Dynamics of a Two-Stage-to-Orbit Vehicle

Christian Zähringer, Gottfried Sachs

TUM Emeriti of Excellence

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

Abstract

Results from wind tunnel tests concerning the separation of a two-stage-to-orbit vehicle are presented. Force and moment characteristics of the orbital stage show significant aerodynamic interference effects between the orbital and the carrier stages. This concerns changes in magnitude as well as dependencies which are solely due to the interference.

Original language	English
Title of host publication	Basic Research and Technologies for Two-Stage-to-Orbit Vehicles
Publisher	John Wiley and Sons
Pages	489-497
Number of pages	9
ISBN (Print)	3527277358, 9783527277353
DOIs	https://doi.org/10.1002/3527605711.ch6
State	Published - 7 Nov 2005

Keywords

Control problems
Flight dynamics
Flight mechanics and control
Optimal trajectories for hypersonic vehicles
Research
Safety improvement
Technologies for two-stage-to-orbit vehicles
Thermal load reduction

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10.1002/3527605711.ch6

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abstract = "Results from wind tunnel tests concerning the separation of a two-stage-to-orbit vehicle are presented. Force and moment characteristics of the orbital stage show significant aerodynamic interference effects between the orbital and the carrier stages. This concerns changes in magnitude as well as dependencies which are solely due to the interference.",

keywords = "Control problems, Flight dynamics, Flight mechanics and control, Optimal trajectories for hypersonic vehicles, Research, Safety improvement, Technologies for two-stage-to-orbit vehicles, Thermal load reduction",

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Flight Mechanics and Control Problems of Two-Stage-to-Orbit Vehicles: Wind Tunnel Tests for Modelling the Separation Dynamics of a Two-Stage-to-Orbit Vehicle. / Zähringer, Christian; Sachs, Gottfried.
Basic Research and Technologies for Two-Stage-to-Orbit Vehicles. John Wiley and Sons, 2005. p. 489-497.

Research output: Chapter in Book/Report/Conference proceeding › Chapter › peer-review

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KW - Flight dynamics

KW - Flight mechanics and control

KW - Optimal trajectories for hypersonic vehicles

KW - Research

KW - Safety improvement

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Flight Mechanics and Control Problems of Two-Stage-to-Orbit Vehicles: Wind Tunnel Tests for Modelling the Separation Dynamics of a Two-Stage-to-Orbit Vehicle

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Keywords

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