DLR Portal
Home
|
Textversion
|
Impressum
|
Sitemap
|
Kontakt
|
Accessibility
Imprint
Privacy
|
Deutsch
You are here:
Home
:
Departments
:
Mechanics and Thermal Systems
:
Department Activities
Advanced Search
Institute
Missionen
Departments
Avionics Systems
Landing and Exploration Systems
Mechanics and Thermal Systems
Department Activities
Research Priorities
Laboratories
Navigation and Control Systems
System Enabling Technologies
System Analysis Space Segment
Space Launcher System Analysis
Systems Engineering and Project Office
Transport and Propulsion Systems
Electronic Laboratory
Laboratories and Test Facilities
News
Events
Jobs & Careers
DLR_School_Lab Bremen
Publications
Department Activities
ReFEX
Das „Reusability Flight Experiment“ (ReFEx) ist ein Technologiedemonstrator für zukünftige geflügelte wiederverwendbare Stufen. Das Modell zeigt ReFEx in seiner Wiedereintrittskonfi guration, nachdem es von seiner Trägerrakete abgesetzt wurde
More
CALLISTO
CALLISTO ist ein wiederverwendbarer Demonstrator für eine Senkrechtstart- und landeraketenstufe (VTVL). CALLISTO wird gemeinsam von DLR, JAXA und CNES entwickelt, gebaut und getestet. Nennenswerte Eigenschaften – im Vergleich zu konventionellen verbrauchbaren Trägerraketen – sind CALLISTOs Landesystem und seine aerodynamischen Steuerungsoberflächen.
More
S2TEP
Mit der Kleinsatelliten-Plattform S2TEP verfügt das DLR über eine unabhängige Plattform zur Durchführung eigener Technologieexperimente unter Weltraumbedingungen.
More
Gossamer-1
The Gossamer-1 project (gossamer, meaning thin and light) aims to develop and create a space-qualified technology for the deployment of ultra-lightweight, large film structures in space.
More
Deployment Systems
As part of the Clean Space roadmap, ESA is researching and developing technologies that will prevent the formation of space debris. The Code of Conduct stipulates that satellites must be deorbited within 25 years of passivation at the end of their useful life.
More
ADEO
As part of the Clean Space roadmap, ESA is researching and developing technologies that will prevent the formation of space debris. The Code of Conduct stipulates that satellites must be deorbited within 25 years after passivation at the end of their useful life.
More
InSight
The core component of HP³ is an instrumented, electromechanical 'mole', equipped with an active, and a passive Thermal Measurement Suite (TEM-A and TEM-P), as well as a combined accelerometer and tiltmeter (ACTIL), which uses an internal hammering mechanism to penetrate through the ground.
More
Copyright © 2021 German Aerospace Center (DLR). All rights reserved.