elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

DLR HABLEG – High Altitude Balloon Launched Experimental Glider

Wlach, Sven and Schwarzbach, Marc and Laiacker, Maximilian (2015) DLR HABLEG – High Altitude Balloon Launched Experimental Glider. In: 22nd ESA Symposium on European Rocket and Balloon Programmes and Related Research (SP-730), pp. 385-392. ESA Communications. 22nd ESA Symposium on European Rocket and Balloon Programmes and Related Research, 7.-12. Juni 2015, Tromsø, Norwegen. ISBN 978-92-9221-294-0 ISSN 1609-042X

[img] PDF (DLR HABLEG – HIGH ALTITUDE BALLOON LAUNCHED EXPERIMENTAL GLIDER)
909kB

Official URL: http://pac.spaceflight.esa.int/data/22nd_ESA_PAC_Symposium_proceedings.pdf

Abstract

The group Flying Robots at the DLR Institute of Robotics and Mechatronics in Oberpfaffenhofen conducts research on solar powered high altitude aircrafts. Due to the high altitude and the almost infinite mission duration, these platforms are also denoted as High Altitude Pseudo-Satellites (HAPS). This paper is about the design, building, integration and testing of a flying experimental platform for high altitudes. This unmanned aircraft, with a wingspan of 3 m and a mass of less than 10 kg, is meant to be launched as a glider from a high altitude balloon in 20 km altitude and shall investigate technologies for future large HAPS platforms. The aerodynamic requirements of high altitude flight were investigated and a design solution to allow for stable flight in the low-density atmosphere was derived. This includes the development of a launch method allowing for a safe transition to horizontal flight from free-fall with low control authority. Due to the harsh environmental conditions in the stratosphere, the integration of electronic components in the airframe is a major effort. Considering thermal suitability and the usage on future HAPS platforms, a concept of housing all major avionics in a single container was devised. For regulatory reasons a reliable and situation dependent flight termination system had to be implemented. A mission simulation and various system tests were developed and used for crew training as well as qualification of the system. Results of flight testing the aircraft will also be presented.

Item URL in elib:https://elib.dlr.de/100773/
Document Type:Conference or Workshop Item (Speech)
Title:DLR HABLEG – High Altitude Balloon Launched Experimental Glider
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Wlach, Svensven.wlach (at) dlr.deUNSPECIFIED
Schwarzbach, Marcmarc.schwarzbach (at) dlr.deUNSPECIFIED
Laiacker, Maximilianmaximilian.laiacker (at) dlr.deUNSPECIFIED
Date:June 2015
Journal or Publication Title:22nd ESA Symposium on European Rocket and Balloon Programmes and Related Research
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 385-392
Publisher:ESA Communications
ISSN:1609-042X
ISBN:978-92-9221-294-0
Status:Published
Keywords:DLR HABLEG – High Altitude Balloon Launched Experimental Glider, Stratosphäre, Stratosphärenflug, High Altitude Pseudo Satellite, Abwurf, UAV, unbemannt, Dauerflug, Solarflugzeug, ELHASPA
Event Title:22nd ESA Symposium on European Rocket and Balloon Programmes and Related Research
Event Location:Tromsø, Norwegen
Event Type:international Conference
Event Dates:7.-12. Juni 2015
Organizer:ESA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Technik für Raumfahrtsysteme
DLR - Research theme (Project):R - Vorhaben Weiterentwicklung Robotik - Mechatronik und Dynamik
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of Robotics and Mechatronics (since 2013) > Mechatronic Components and Systems
Deposited By: Wlach, Sven
Deposited On:15 Dec 2015 11:17
Last Modified:31 Jul 2019 19:58

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.