THE DLR ORBITAL HUB: A CONCURRENT ENGINEERED POST-ISS APPROACH
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1 THE DLR ORBITAL HUB: A CONCURRENT ENGINEERED POST-ISS APPROACH
2 Folie 2 > Orbital-Hub > O. Romberg, Oct 2016 THE DLR ORBITAL HUB: A CONCURRENT ENGINEERED POST-ISS APPROACH 7th International Conference on Systems & Concurrent Engineering for Space Applications SECESA 2016 Madrid, 5th to 7th October 2016 Institut für Raumfahrtsysteme Systemanalyse Raumsegment Oliver Romberg Dominik Quantius Antonio Martelo Stephan Jahnke Hansjörg Dittus Sven Baerwalde Hans Schlegel Mike Gold George Zumka Ingo Retat Rainer Wohlgemuth Max. Lange
3 Folie 3 > Orbital-Hub > O. Romberg, Oct 2016 THE DLR ORBITAL HUB: A CONCURRENT ENGINEERED POST-ISS APPROACH 7th International Conference on Systems & Concurrent Engineering for Space Applications SECESA 2016 Madrid, 5th to 7th October 2016 Institut für Raumfahrtsysteme Systemanalyse Raumsegment Content: Introduction Goal of CE - Studies Concurrent Design of the Orbital Hub Conclusions
4 Folie 5 > Orbital-Hub > O. Romberg, Oct 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 to be worked out in a series of CE - studies
5 Folie 6 > Orbital-Hub > O. Romberg, Oct 2016 Orbital-Hub Concept Development CEF at DLR Bremen: Simultaneous Design Laboratory Based on S/W: Virtual Satellite 3 rooms, 25 work stations Moderated process based on sessions / off-line work Output: Phase 0/A - level After concept trade: Orbital Hub designed in a series of 3 CE studies (1 week each) 1. User Requirements & P/L - study a. o. with scientists 2. Base Platform design with users, scientists & astronauts co-op 3. Free-Flyer as first H/W realization with add. industry co-op
6 Folie 8 > Orbital-Hub > O. Romberg, Oct 2016 Base Platform n Free-Flyer design CE- Study participation of various DLR ISS experienced scientists/experts NASA and ESA astronauts Bigelow Aerospace Airbus-DS 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
7 Folie 9 > Orbital-Hub > O. Romberg, Oct 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!
8 Folie 10 > Orbital-Hub > O. Romberg, Oct 2016 Engineering Concept for Modular LEO Platform Modular Orbital-Hub: Dockable Module/Platform as an European Initiative
9 Folie 11 > Orbital-Hub > O. Romberg, Oct 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
10 Folie 14 > Orbital-Hub > O. Romberg, Oct 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 Series of CE-Studies based on VirSat -> Modular Orbital-Hub involving scientists, astronauts, space industry (ADS, Bigelow) 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)
11 Folie 15 > Orbital-Hub > O. Romberg, Oct 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
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