| Nome |
# |
|
Thermal design and analysis of a nanosatellite in low earth orbit, file e384c42e-572d-d4b2-e053-9f05fe0a1d67
|
1.293
|
|
Design of all electric secondary power system for future advanced MALE UAV, file e384c42e-1803-d4b2-e053-9f05fe0a1d67
|
1.139
|
|
Conceptual design of a habitation module for a deep space exploration mission, file e384c42e-1cc7-d4b2-e053-9f05fe0a1d67
|
1.034
|
|
Active space debris removal by a hybrid propulsion module, file e384c42e-27f5-d4b2-e053-9f05fe0a1d67
|
842
|
|
Rational and affordable concepts of Landing Gear for small reentry vehicle demonstrators, file e384c42e-1f38-d4b2-e053-9f05fe0a1d67
|
618
|
|
Integration of different MBSE approaches within the design of a control maintenance system applied to the aircraft fuel system, file e384c42f-53e3-d4b2-e053-9f05fe0a1d67
|
571
|
|
Diesel Engine Application on AEW&C Turboprop Effectiveness-Cost Assessment, file e384c42e-120f-d4b2-e053-9f05fe0a1d67
|
520
|
|
Reusable space tug concept and mission, file e384c42f-2ec3-d4b2-e053-9f05fe0a1d67
|
519
|
|
Interplanetary CubeSats system for space weather evaluations and technology demonstration, file e384c42e-35a5-d4b2-e053-9f05fe0a1d67
|
518
|
|
Development and Validation of on-board systems control laws, file e384c42e-175a-d4b2-e053-9f05fe0a1d67
|
505
|
|
A methodology for innovative technologies roadmaps assessment to support strategic decisions for future space exploration., file e384c42e-2d82-d4b2-e053-9f05fe0a1d67
|
477
|
|
A case study for spacegate point-to-point transportation: Evaluation of a reference end-to-end mission operations and assessment of the associated safety aspects, file e384c42f-2f5b-d4b2-e053-9f05fe0a1d67
|
334
|
|
Cost estimation methodology and tool for future Reusable Access To Space Systems, file e1052032-65f9-42f9-a566-f1e904bb4028
|
322
|
|
MBSE approach to support and formalize mission alternatives generation and selection processes for hypersonic and suborbital transportation systems, file e384c42f-e0d8-d4b2-e053-9f05fe0a1d67
|
310
|
|
Autonomous take-off and landing for unmanned aircraft system: Risk and safety analysis, file e384c42e-8160-d4b2-e053-9f05fe0a1d67
|
301
|
|
A methodology to support strategic decisions in future human space exploration: from scenario definition to building blocks assessment, file e384c42e-27f1-d4b2-e053-9f05fe0a1d67
|
296
|
|
Mini-uav remote control: a case study at Politecnico di Torino, file e384c42d-f4e6-d4b2-e053-9f05fe0a1d67
|
277
|
|
Design Of A Reusable Space Tug, file e384c42e-f41f-d4b2-e053-9f05fe0a1d67
|
275
|
|
Active space debris removal by hybrid engine module, file e384c42f-2f2b-d4b2-e053-9f05fe0a1d67
|
265
|
|
Cost-Estimating Model for Aircraft Maintenance, file e384c42f-efbe-d4b2-e053-9f05fe0a1d67
|
241
|
|
FUTURE SPACE EXPLORATION: FROM REFERENCE SCENARIO DEFINITION TO KEY TECHNOLOGIES ROADMAPS, file e384c42e-1c5e-d4b2-e053-9f05fe0a1d67
|
239
|
|
HUMAN EXPEDITION TO A NEAR EARTH ASTEROID: REFERENCE MISSION AND TECHNOLOGIES, file e384c42e-1e97-d4b2-e053-9f05fe0a1d67
|
221
|
|
SEEDS – THE INTERNATIONAL MASTER PROGRAM FOR PREPARING THE YOUNG SYSTEMS ENGINEERS FOR SPACE EXPLORATION, file e384c42e-21ba-d4b2-e053-9f05fe0a1d67
|
218
|
|
Feasibility Study of a Technological Demonstrator of Reduced Size for Sub-Orbital Flight, file e384c42d-e0fe-d4b2-e053-9f05fe0a1d67
|
209
|
|
A model-based approach to the preliminary design of a space tug aimed at early requirement's verification, file e384c42f-cc0d-d4b2-e053-9f05fe0a1d67
|
186
|
|
SET, A SCENARIO EVALUATOR TOOL FOR SUPPORTING SPACE-EXPLORATION MISSION-ARCHITECTURE DESIGN, file e384c42e-1c68-d4b2-e053-9f05fe0a1d67
|
175
|
|
Design, Development and Test of Engineering Models of Tethered Nanosatellites to Observe the Solar Corona, file e384c42e-21ee-d4b2-e053-9f05fe0a1d67
|
170
|
|
Active debris removal space mission concepts based on hybrid propulsion, file e384c42f-2f5c-d4b2-e053-9f05fe0a1d67
|
162
|
|
Effective methodologies to derive strategic decisions from ESA technology roadmaps, file e384c42f-2ec4-d4b2-e053-9f05fe0a1d67
|
161
|
|
A methodology for preliminary sizing of a Thermal and Energy Management System for a hypersonic vehicle, file e384c432-355b-d4b2-e053-9f05fe0a1d67
|
143
|
|
A methodology for preliminary sizing of a Thermal and Energy Management System for a hypersonic vehicle, file e384c431-a3a5-d4b2-e053-9f05fe0a1d67
|
127
|
|
Analysis of a Moon outpost for Mars enabling technologies through a Virtual Reality environment, file e384c42f-ddb3-d4b2-e053-9f05fe0a1d67
|
124
|
|
A trade-off methodology for micro-launchers, file e384c433-c6d8-d4b2-e053-9f05fe0a1d67
|
124
|
|
Innovative Multiple Matching Charts approach to support the conceptual design of hypersonic vehicles, file e384c432-45a6-d4b2-e053-9f05fe0a1d67
|
97
|
|
Spaceport and Ground Segment assessment for enabling operations of suborbital transportation systems in the Italian territory, file e384c432-416c-d4b2-e053-9f05fe0a1d67
|
73
|
|
Life cycle cost estimation for high-speed transportation systems, file e384c431-8db8-d4b2-e053-9f05fe0a1d67
|
71
|
|
Earth-Mars cyclers for a sustainable human exploration of Mars, file e384c432-355c-d4b2-e053-9f05fe0a1d67
|
64
|
|
A NOVEL APPROACH TO PLANETARY ROVER GUIDANCE, NAVIGATION AND CONTROL BASED ON THE ESTIMATION OF THEREMAINING USEFUL LIFE, file e384c432-479d-d4b2-e053-9f05fe0a1d67
|
58
|
|
A conceptual design tool to support high-speed vehicle design, file e384c433-343b-d4b2-e053-9f05fe0a1d67
|
49
|
|
Deep space transportation enhanced by 20 kW-Class Hall Thrusters, file e384c432-31bf-d4b2-e053-9f05fe0a1d67
|
47
|
|
End-to-end approach to flexible and sustainable commercial spaceflight initiatives: Evaluation of operational scenarios, safety aspects, spaceports and associated economic elements, file e384c432-6eeb-d4b2-e053-9f05fe0a1d67
|
42
|
|
Space systems engineering tools for technology roadmapping activities: TrIS, technology roadmapping strategy, and HyDaT, database on hypersonic transportation systems, file e384c432-31f3-d4b2-e053-9f05fe0a1d67
|
40
|
|
EPS architecture analysis for future highpower missions, file e384c432-7830-d4b2-e053-9f05fe0a1d67
|
37
|
|
Influence of high level requirements in aircraft design: From scratch to sketch, file e384c432-7d30-d4b2-e053-9f05fe0a1d67
|
35
|
|
Innovative time-based separation procedures for civil RPAS integration, file e384c432-41cd-d4b2-e053-9f05fe0a1d67
|
33
|
|
Economic and environmental sustainability of liquid hydrogen fuel for hypersonic transportation systems, file e384c432-5ac4-d4b2-e053-9f05fe0a1d67
|
29
|
|
H2020 STRATOFLY Project: from Europe to Australia in less than 3 hours, file e384c434-23d3-d4b2-e053-9f05fe0a1d67
|
29
|
|
Life cycle cost estimation methodology for hypersonic transportation systems, file e384c431-59e3-d4b2-e053-9f05fe0a1d67
|
28
|
|
The selection of an electric propulsion subsystem architecture for high-power space missions, file e384c432-7df0-d4b2-e053-9f05fe0a1d67
|
28
|
|
iDREAM: a multidisciplinary methodology and integrated toolset for flight vehicle engineering, file 15dcf6f0-b8ea-4248-83ed-774e4c1ff074
|
26
|
|
Using the ESA exploration technology roadmaps in support of new mission concepts and technology prioritization, file e384c432-5f37-d4b2-e053-9f05fe0a1d67
|
25
|
|
Aerodynamic characterization of hypersonic transportation systems and its impact on mission analysis, file e384c434-1fb0-d4b2-e053-9f05fe0a1d67
|
25
|
|
Towards a methodology for new technologies assessment in aircraft operating cost, file e384c432-d6d0-d4b2-e053-9f05fe0a1d67
|
24
|
|
Academic Course in Aircraft conceptual design and on-board systems preliminary design at Politecnico di Torino, file e384c42e-8035-d4b2-e053-9f05fe0a1d67
|
22
|
|
Human lunar lander system design, cost estimation and technology roadmaps, file 6a9ea798-fa3b-4d11-8a3e-492c5376b219
|
20
|
|
Technology RoadmappIng Strategy, TRIS: Methodology and tool for technology roadmaps for hypersonic and re-entry space transportation systems, file e384c432-8aca-d4b2-e053-9f05fe0a1d67
|
18
|
|
Sustainable supersonic fuel flow method: An evolution of the boeing fuel flow method for supersonic aircraft using sustainable aviation fuels, file e384c434-45a0-d4b2-e053-9f05fe0a1d67
|
18
|
|
Strategies for preliminary re-design of a LH2 Mach 5 cruiser concept originally conceived for Mach 8 mission, file e384c434-7bff-d4b2-e053-9f05fe0a1d67
|
18
|
|
Integration of an increasing-fidelity aerodynamic modelling approach in the conceptual design of hypersonic cruiser, file e384c434-3054-d4b2-e053-9f05fe0a1d67
|
17
|
|
Thermal Protection System preliminary design of STRATOFLY high-speed propelled vehicle, file e384c434-0464-d4b2-e053-9f05fe0a1d67
|
16
|
|
Technology roadmapping methodology for future hypersonic transportation systems, file e384c434-7eea-d4b2-e053-9f05fe0a1d67
|
16
|
|
STRATOFLY MR3 – how to reduce the environmental impact of high-speed transportation, file e384c434-b552-d4b2-e053-9f05fe0a1d67
|
16
|
|
Advanced European Re-Entry System Based on Inflatable Heat Shields Technology Roadmap and Technical challenges (EFESTO project), file e384c433-572a-d4b2-e053-9f05fe0a1d67
|
15
|
|
Research, development and production costs prediction parametric model for future civil hypersonic aircraft, file 75f3d8a7-5233-475e-9c02-41847db14c34
|
14
|
|
Application of MBSE to model Hierarchical AI Planning problems in HDDL, file e384c433-d98a-d4b2-e053-9f05fe0a1d67
|
14
|
|
Life Cycle Cost estimation for future reusable access to space systems, file e384c434-454b-d4b2-e053-9f05fe0a1d67
|
13
|
|
Rapid prototyping for Martian space systems, file 8391f3e5-2fa6-4338-b0a1-a65285b6b875
|
12
|
|
Application of a hierarchical task planner to a lunar lava tube analogue robotic mission, file e384c434-44a5-d4b2-e053-9f05fe0a1d67
|
12
|
|
High level requirements impact on configuration trade-off analyses in a multidisciplinary integrated conceptual design methodology, file e384c432-7773-d4b2-e053-9f05fe0a1d67
|
11
|
|
Performance Assessment of an Integrated Environmental Control System of Civil Hypersonic Vehicles, file e384c434-bd30-d4b2-e053-9f05fe0a1d67
|
11
|
|
Technology roadmaps for the development of future high-speed transportation systems, file e384c434-23d5-d4b2-e053-9f05fe0a1d67
|
10
|
|
Preliminary Design and Simulation of a Thermal Management System with Integrated Secondary Power Generation Capability for a Mach 8 Aircraft Concept Exploiting Liquid Hydrogen, file c6a3462e-4025-4153-b664-a761cb352a39
|
9
|
|
Preliminary reliability and safety assessment methodology for trans-atmospheric transportation systems, file e384c432-333c-d4b2-e053-9f05fe0a1d67
|
8
|
|
Simulating Operational Concepts for Autonomous Robotic Space Exploration Systems: A Framework for Early Design Validation, file e90df3da-052a-4225-b72d-86c35494b23f
|
8
|
|
Liquid Metals Heat-Pipe solution for hypersonic air-intake leading edge: Conceptual design, numerical analysis and verification, file e384c434-cf90-d4b2-e053-9f05fe0a1d67
|
7
|
|
Flight Control System Design and Sizing Methodology for hypersonic cruiser, file f1395643-fb36-48d4-ac20-74b8ff99e2f0
|
7
|
|
An Approach to the Preliminary Sizing and Performance Assessment of Spaceplanes’ Landing Parafoils, file abe4234a-47a8-4694-bfc6-ec3642d5e2f8
|
6
|
|
STRATOFLY MR3 – how to reduce the environmental impact of high-speed transportation, file e384c434-3055-d4b2-e053-9f05fe0a1d67
|
6
|
|
Life cycle cost estimation for high-speed transportation systems, file e384c431-3239-d4b2-e053-9f05fe0a1d67
|
5
|
|
Italian approach to suborbital space transportation: From setup of harmonized framework to spaceport and ground segment evaluation for enabling operations in the Italian territory, file e384c432-8401-d4b2-e053-9f05fe0a1d67
|
5
|
|
A conceptual design tool to support high-speed vehicle design, file e384c433-2961-d4b2-e053-9f05fe0a1d67
|
5
|
|
Strategies for preliminary re-design of a LH2 Mach 5 cruiser concept originally conceived for Mach 8 mission, file e384c434-454c-d4b2-e053-9f05fe0a1d67
|
5
|
|
Conceptual design emissions evaluation
for the STRATOFLY MR3 vehicle, file 3a984569-c746-4561-a7e1-ddc283e3125e
|
4
|
|
Heuristic and exact techniques for aircraft maintenance scheduling, file e384c42e-0a25-d4b2-e053-9f05fe0a1d67
|
4
|
|
Human life support in permanent lunar base architectures, file e384c42e-328d-d4b2-e053-9f05fe0a1d67
|
4
|
|
A Virtual Reality approach for studying a future human lunar outpost: an integrated simulation case study of a Stand Alone Power System, file e384c42f-c0b7-d4b2-e053-9f05fe0a1d67
|
4
|
|
A methodology for preliminary sizing of a Thermal and Energy Management System for a hypersonic vehicle, file e384c431-c944-d4b2-e053-9f05fe0a1d67
|
4
|
|
Multidisciplinary mission and system design tool for a reusable electric propulsion space tug, file e384c432-5701-d4b2-e053-9f05fe0a1d67
|
4
|
|
Thermal design of heat pipe cooling systems: conceptual design and numerical development, file fb315f52-8009-4873-9fa7-8cfaf995e6f9
|
4
|
|
Aero-thermal design of STRATOFLY MR3 hypersonic vehicle, file 213ebd48-7f27-49bd-b85e-49b1f55ff6c4
|
3
|
|
Microlauncher design, cost estimation and technology roadmaps, file 463b87a2-dfdf-4554-b301-cada384863e8
|
3
|
|
Propellant subsystem design for hypersonic cruiser exploiting liquid hydrogen, file 54a2607e-e1d5-4e06-b261-06f63504cb73
|
3
|
|
Zonal safety analysis in aircraft conceptual design: application to SAvE aircraft, file e384c42e-1cc3-d4b2-e053-9f05fe0a1d67
|
3
|
|
Applied design methodology for lunar rover elastic wheel, file e384c42e-1cc5-d4b2-e053-9f05fe0a1d67
|
3
|
|
Incremental architectures for a permanent human lunar outpost with focus on isru technologies., file e384c42e-328e-d4b2-e053-9f05fe0a1d67
|
3
|
|
PRELIMINARY DESIGN AND SIZING OF A CABIN ESCAPE SYSTEM FOR A SUBORBITAL VEHICLE AIMED AT PARABOLIC FLIGHTS, file e384c42f-4241-d4b2-e053-9f05fe0a1d67
|
3
|
|
Virtual Reality to assist the engineering decision-making process: improving the Concurrent Design approach, file e384c42f-c361-d4b2-e053-9f05fe0a1d67
|
3
|
|
EUROPEAN FLEXIBLE HEAT SHIELDS:
ADVANCED TPS DESIGN AND TESTS FOR FUTURE IN-ORBIT DEMONSTRATION, file e384c432-74d8-d4b2-e053-9f05fe0a1d67
|
3
|
|
Methodology for requirements definition of complex space missions and systems, file e384c433-2a49-d4b2-e053-9f05fe0a1d67
|
3
|
|
Application of a hierarchical task planner to a lunar lava tube analogue robotic mission, file e384c434-5a93-d4b2-e053-9f05fe0a1d67
|
3
|
| Totale |
14.181 |
Archivio Istituzionale della Ricerca