{"id":2690,"date":"2015-06-28T02:31:08","date_gmt":"2015-06-28T00:31:08","guid":{"rendered":"http:\/\/www.hps-gmbh.com\/en\/?page_id=2690"},"modified":"2020-05-12T00:45:49","modified_gmt":"2020-05-11T22:45:49","slug":"success-trajectory-2","status":"publish","type":"page","link":"https:\/\/www.hps-gmbh.com\/en\/portfolio\/subsystem-elements\/success-trajectory-2\/","title":{"rendered":"Success Trajectory"},"content":{"rendered":"

[vc_row full_width=”” parallax=”” parallax_image=””][vc_column width=”1\/1″][vc_row_inner][vc_column_inner el_class=”” width=”1\/1″][vc_column_text]Subsystem Elements<\/span>
\n Die Zuordnung der Projekte bezieht sich auf das Jahr der Beauftragung.<\/span>[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][\/vc_column][\/vc_row][vc_row el_class=”timeline”][vc_column width=”5\/12″ css=”.vc_custom_1434471522108{margin-bottom: 15px !important;}”][vc_column_text]<\/p>\n

2018<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-66″]3D-Honeycomb:<\/strong> Application Inputs to the Development of 3D-Curved Honeycombs for Spacecraft Structures
\n2018-2018[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-67″]HICCS:<\/strong> Application Inputs (Antenna Subreflector) to the Development of Highly Integral Carbon-SMC-Components for Satellites
\n2018-2019[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text]<\/p>\n

2017<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-65″]TRISTAN-C:<\/strong> Development of Technology for Integration of Electronics into non-metal Satellite Structures
\n2017-2019[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-64″]A3LUB:<\/strong> Application Inputs (LDRS-Components) to the Development of Highly Efficient Dry Lubricants
\n2017-2019[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-63″]SPOTLITE:<\/strong> Feasibility Study on 3D-Printed Multi-Material Radiation Shielding Components
\n2017-2019[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-62″]3D-PAN:<\/strong> Feasibility Study on 3D-Printed Ka-Band Titanium Reflector Antenna for Earth Observation Applications
\n2017-2018[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text css_animation=””]<\/p>\n

2016<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-61″]NATAP:<\/strong> Carbon Nanotube Technology and Material Engineering for Various Space Applications such as Feed Horns and Optical Mirrors
\n2016-2018[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text css_animation=””]<\/p>\n

2015<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text css_animation=”” el_class=”suc-traj success-60″]CALM:<\/strong> Investigation of Applicability of Additive Layer Manufacturing (ALM) for Secondary Spacecraft Structures
\n2015-2017[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text css_animation=””]<\/p>\n

2014<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text css_animation=”” el_class=”suc-traj success-59″]RAPRO:<\/strong> Design, manufacture and test of novel multi-layered radiation shielding materials for protection of spacecraft electronics or other sensitive equipment
\n2014-2019[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text css_animation=”” el_class=”suc-traj success-01″]RAPRO:<\/strong> Conceptual and Experimental Evaluation of Lighter and More Efficient Radiation Protection for Electronics and Sensitive Parts
\n2014\u20132016[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text]<\/p>\n

2013<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-58″]RTM-E-BOX:<\/strong> Development of Thermally Conductive CFRP Material for Electronic Housings
\n2013-2015[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text css_animation=”” el_class=”suc-traj success-02″]NAFO:<\/strong> Use of Nanocomposite Reinforced Foams for Manufacture of Superlightwight Stiff Sandwich Panels
\n2013\u20132015[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-03″]AMOF:<\/strong> Ablative Material Optimisation & Definition of Material Families Adaptable to Various Re-entry Application
\n2013\u20132015[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-04″]RTM-CFRP:<\/strong> Highly Thermally Conductive CFRP Electronic Housings Produced via RTM Technology; HPS: reference housing selection, design and analysis
\n2013\u20132015[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text]<\/p>\n

2011<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-05″]NACO2:<\/strong> Non-Conventional Matrix\/CNT Reinforced Composite for Application in Space Part 2
\n2011\u20132014[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text]<\/p>\n

2010<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-57″]VANESSA:<\/strong> Validation of Numerical Engineering Simulations: Standardization Actions
\n2010-2013[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text css_animation=”” el_class=”suc-traj success-56″]NAREMA:<\/strong> Nanotube-Reinforced Structural Materials for Spacecraft Applications
\n2010-2012[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text css_animation=”” el_class=”suc-traj success-06″]NARE:<\/strong> Nanotube Reinforced Structural Materials for Spacecraft Applications
\n2010\u20132012[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-07″]VEMS:<\/strong> Thermal Protection for an External Camera Onboard VEGA Launcher; Prime: HPS-PT, HPS-D: engineering support
\n2010\u20132012[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text]<\/p>\n

2009<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-08″]ECUD:<\/strong> CFRP Electronic Housing Prototype for Aircraft Applications
\n2009\u20132011[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-09″]CARBOSPACE:<\/strong> CFRP Electronic Housings Doped by CNT Material \u00a0for Space Application
\n2009\u20132012[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-10″]LISE:<\/strong> Lightweight Flight Sensors & Measurement Techniques for Re-entry Spacecrafts
\n2009\u20132011[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text]<\/p>\n

2008<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-11″]DEAM:<\/strong> Development of an European Ablative Material for Heatshields of Sample Return Missions
\n2008\u20132012[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-55″]AMOD:<\/strong> Management and Thermal Engineering for Aerochemistry Models for Re-entry Spacecraft
\n2008-2011[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text css_animation=”” el_class=”suc-traj success-50″]COPE:<\/strong> Carbon nano-species (CNT, CNF) for modified polymer composites and Carbon foams for sandwich cores
\n2008-2011[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-12″]C-FILM:<\/strong> Highly Conductive Carbon Films for Electronic Boards for Space Apllications
\n2008\u20132010[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text]<\/p>\n

2007<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-13″]CCORE:<\/strong> European CFRP Honeycomb Material; HPS: space applications and requirements
\n2007\u20132012[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-54″]ADVISE:<\/strong> Advanced Dynamic Validations using Integrated Simulation and Experimentation
\n2007-2011[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-53″]SpaceRTM E-Box:<\/strong> Verification of Resin Transfer Moulding (RTM) as Alternative for Electronic Housing Manufacturing
\n2007-2009[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text css_animation=”” el_class=”suc-traj success-14″]NACO:<\/strong> Non-Conventional Matrix \/ CNT Composites for Space Application
\n2007\u20132009[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-15″]NANO:<\/strong> Improvement of Thermal Dissipation of Glues by Nano-Material
\n2007\u20132009[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-16″]ISAS:<\/strong> RF-Invisible Struts for Antenna Systems
\n2007\u20132012[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-17″]DUST:<\/strong> Experimental Statistic Enhancement of Data for Mars Dust Effects on Spacecraft Ablators
\n2007\u20132010[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text]<\/p>\n

2006<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-52″]BOJO:<\/strong> Management of the Development of Hybrid CFRP-Titanium Laminates Reinforcing Bolted Interfaces
\n2006-2009[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text css_animation=”” el_class=”suc-traj success-18″]MDUST:<\/strong> Experimental and Theoretical Study of Mars Dust Effects on Spacecraft Ablators
\n2006\u20132007[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-19″]SRTM:<\/strong> CNT-Doped Space Components Manufactured by RTM-Technology; HPS: design and analysis of CFRP electronic housing
\n2006\u20132009[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text]<\/p>\n

2005<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-20″]EMI:<\/strong> Spacecraft EMI Control in the Presence of Composite Material
\n2005\u20132008[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-21″]CNTM:<\/strong> Nanotube Composite Materials Based on Polymer, Ceramic and Metal Matrices
\n2005\u20132009[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text]<\/p>\n

2003<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-22″]IHS:<\/strong> High Temperature Re-Usable Insulation for Hot Structures of Re-entry Spacecrafts
\n2003\u20132006[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-23″]STPS:<\/strong> Smart Thermal Protection Systems for Re-usable Re-entry Spacecrafts
\n2003\u20132006[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_column_text]<\/p>\n

2002<\/h3>\n

[\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-51″]FAILURE CRITERIA:<\/strong> Investigation of Failure Criteria of CFRP- and Ceramic Components via Sample Testing and Correlation with Analysis
\n2002-2005[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][\/vc_column][vc_column width=”7\/12″][vc_single_image image=”1184″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-01″][vc_single_image image=”2149″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-02″][vc_single_image image=”2134″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-03″][vc_single_image image=”2153″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-04″][vc_single_image image=”2147″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-05″][vc_single_image image=”2151″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-06″][vc_single_image image=”2156″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-07″][vc_single_image image=”2294″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-08″][vc_single_image image=”2136″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-09″][vc_single_image image=”2145″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-10″][vc_single_image image=”2139″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-11″][vc_single_image image=”2135″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-12″][vc_single_image image=”2137″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-13″][vc_single_image image=”2148″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-14″][vc_single_image image=”2150″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-15″][vc_single_image image=”2144″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-16″][vc_single_image image=”2140″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-17″][vc_single_image image=”2146″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-18″][vc_single_image image=”2154″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-19″][vc_single_image image=”2142″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-20″][vc_single_image image=”2138″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-21″][vc_single_image image=”2157″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-22″][vc_single_image image=”2155″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-23″][vc_single_image image=”3704″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-50″][vc_single_image image=”3707″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-51″][vc_single_image image=”3708″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-52″][vc_single_image image=”3710″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-53″][vc_single_image image=”3709″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-54″][vc_single_image image=”3711″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-55″][vc_single_image image=”3712″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-56″][vc_single_image image=”3713″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-57″][vc_single_image image=”3967″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-58″][vc_single_image image=”3715″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-59″][vc_single_image image=”3716″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-60″][vc_single_image image=”3717″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-61″][vc_single_image image=”3718″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-62″][vc_single_image image=”3719″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-63″][vc_single_image image=”3720″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-65″][vc_single_image image=”3723″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-66″][vc_single_image image=”3722″ border_color=”grey” img_link_large=”” img_link_target=”_self” img_size=”trajectory” el_class=”suc-traj-img success-67″][\/vc_column][\/vc_row]<\/p>\n<\/section>","protected":false},"excerpt":{"rendered":"

[vc_row full_width=”” parallax=”” parallax_image=””][vc_column width=”1\/1″][vc_row_inner][vc_column_inner el_class=”” width=”1\/1″][vc_column_text]Subsystem Elements Die Zuordnung der Projekte bezieht sich auf das Jahr der Beauftragung.[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][\/vc_column][\/vc_row][vc_row el_class=”timeline”][vc_column width=”5\/12″ css=”.vc_custom_1434471522108{margin-bottom: 15px !important;}”][vc_column_text] 2018 [\/vc_column_text][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-66″]3D-Honeycomb: Application Inputs to the Development of 3D-Curved Honeycombs for Spacecraft Structures 2018-2018[\/vc_column_text][\/vc_column_inner][\/vc_row_inner][vc_row_inner el_id=””][vc_column_inner el_class=”” width=”1\/1″][vc_column_text el_class=”suc-traj success-67″]HICCS: Application Inputs (Antenna Subreflector) to the Development […]<\/p>\n","protected":false},"author":1,"featured_media":0,"parent":2618,"menu_order":4,"comment_status":"open","ping_status":"closed","template":"nobg.php","meta":[],"acf":[],"yoast_head":"\nSuccess Trajectory - 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