Modular Low Earth Orbital-Hub DLR Vision 2025
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1 The Space Congress Proceedings 2016 (44th) The Journey: Further Exploration for Universal Opportunities May 25th, 10:45 AM Modular Low Earth Orbital-Hub DLR Vision 2025 Dr. Oliver Romberg German Space Center (DLR), Bremen Follow this and additional works at: Scholarly Commons Citation Romberg, Dr. Oliver, "Modular Low Earth Orbital-Hub DLR Vision 2025" (2016). The Space Congress Proceedings This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact
2 Modular Low Earth Orbital-Hub DLR Vision 2025
3 Folie 2 > Orbital-Hub > O. Romberg, May 2016 Low Earth Orbital-Hub DLR Vision th Space Congress, Cape Canaveral, Florida May 24-26, 2016 Institut für Raumfahrtsysteme Systemanalyse Raumsegment Dr. Oliver Romberg
4 Folie 3 > Orbital-Hub > O. Romberg, May 2016 Low Earth Orbital-Hub DLR Vision th Space Congress, Cape Canaveral, Florida May 24-26, 2016 Content: Introduction Project Goal O-Hub Concept Conclusions
5 Folie 4 > Orbital-Hub > O. Romberg, May 2016 Institute of Space Systems / Bremen Studies and analyses of launch vehicles and orbital systems to evaluate their technical performance and costs Design and development of spacecraft / missions (small satellites, lander vehicle) Development of technologies for - Cryogenic Propellant Management - Planetary Landing - Satellite Subsystems - Guidance Navigation and Control - High Precision Optical Measurements - Habitation & Life-Support-Systems
6 Folie 5 > Orbital-Hub > O. Romberg, May 2016 Project Goal Modular Orbital-Hub Proposals for the German/European position to continue manned spaceflight in LEO (Outpost, Observatory) after ISS-operation based on benefit of human presence in space
7 Folie 6 > Orbital-Hub > O. Romberg, May 2016 Orbital-Hub Concept Development Various DLR ISS experienced scientists/experts plus NASA and ESA Astronauts, Bigelow Aerospace, Airbus-DS participated in simultaneous design studies (Concurrent Engineering Studies) Result: Modular, simple but extendible platform with Free-Flyer DLR s Orbital-Hub concept with Free-Flyer consisting of external science platform and pressurized laboratory
8 Folie 7 > Orbital-Hub > O. Romberg, May 2016 Orbital-Hub Concept Development Simultaneous Design Laboratory Based on S/W Virtual Satellite Simultaneous involvement of experts for 1-2 weeks Common understanding Result: Mature Phase 0/A concept Outputs: Proposals for next phase
9 Folie 8 > Orbital-Hub > O. Romberg, May 2016 Concept Development with Scientists in DLR CEF Participating Disciplines - Science Coordination - Architecture / Configuration - Payload, I/Fs - Material Physics - Earth Observation - Atmosphere Physics - Human Physiology - Gravitation Biology - Radiation Biology - Technology Demonstration / Expl. - Operations - Robotics - Astronomy / Astrophysics - To be added: Plasma Physics tbd
10 Folie 9 > Orbital-Hub > O. Romberg, May 2016 Main Objectives for Development Significant cost reduction (lessons learnt from ISS), small concept! Utilization of O-Hub as platform for Earth Observation Technology Demonstration Commercial users (involvment of global players, private investments) Science (following to ISS but with Free Flyer) Exploration Preparation (crew-training for planetary missions, mission simulation) High flexible, modular and extendible concept ( Space Village ) Involving worldwide roadmaps, synergy potentials with existing systems (e. g. Dream Chaser, Space Exploration, ) Keeping human spaceflight alive (in EU / D)! More self-standing and dominant role for Europe/Germany in Space!
11 Folie 10 > Orbital-Hub > O. Romberg, May 2016 Engineering Concepts for Modular LEO Platform Modular Orbital-Hub: Dockable Module/Platform as a European Initiative
12 Folie 11 > Orbital-Hub > O. Romberg, May 2016 Orbital-Hub Free-Flyer Spacecraft: launch mass: 18.7 t (w/o payload) propulsion: hybrid (chemical / electrical) diameter: 4.5 m length: 15.4 m power: 20 kw average Features: external decoupled Observation / Science Platform modular, scalable and attitude-flexible concept crew operation while docked at O-Hub / capsule / ISS transport by single A64-Launch low cost to be realised within ~8 years
13 Folie 14 > Orbital-Hub > O. Romberg, May 2016 Conclusions and Next Steps Further motivation and justification (beyond science) to build and operate human-tended infrastructures in LEO High interest of possible users in Mini-Station with free flyer i. e. Modular Orbital-Hub involving space industry (ADS, Bigelow) Involvement of German key contributions for further consideration Astronautical spaceflight in LEO Ongoing requirements definition with int. community Automated service modules, habitation modules Robotic technology options Advanced low thrust propulsion Operations Major Next Steps: Detailled Design of O-Hub Free-Flyer Module in co-op with ADS Detailed definition of use cases with international partners (commercial, industry, agencies, institutions)
14 Folie 15 > Orbital-Hub > O. Romberg, Mai 2016 Thank you for your interest! April 2016 O. Romberg, D. Quantius, S. Baerwalde, H. Dittus et al. Institute of Space Systems System Analysis Space Segment
THE DLR ORBITAL HUB: A CONCURRENT ENGINEERED POST-ISS APPROACH
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