session 3
Modern Day Space Elevator Transformational Strengths and their Applications
- type
oral
- Description
Modern Day Space Elevator design concepts are driven from many arenas. The customer is of course the first driver of design for the future; however, the transformational strengths determine the mission fulfillment. Once the 100,000 km tether is in place and the tether climbers start raising customer payloads, the remarkable characteristics will start to dominate the movement of mass for customers. This symposia will address how the following characteristics impact mission success for the customers: (a) Unmatched efficiencies with daily, routine, safe, and inexpensive delivery of logistics payloads, (b) Unmatched massive movement (initial operational capability (IOC) at 30,000 tonnes/yr with full operational capability (FOC) 170,000 tonnes/yr), (c) Unmatched velocity (starting at 7.76 km/sec at 100,000 altitude enables rapid transits to the Moon, Mars and beyond), (d), Ensures environmentally neutral operations as a green road to space, (e) Reduces rocket fairing design limitations, (f) Assembly at the top of the gravity well, and (g) Transforming the economic strengths of strategic investment, ubiquitous access, and uninterrupted exchange of resources. The Keynote Speech for this technical session will be entitled the "Jerome Pearson Memorial Lecture."
- Date
2024-10-15
- Time
- Room
- IPC members
Co-Chair: Dr. Peter Swan, Space Elevator Development Corporation, United States;
Co-Chair: Dr. Yoji Ishikawa, Obayashi Corporation, Japan;
Rapporteur: Mr. Daniel Griffin, Royal Institute of Technology (KTH), Sweden;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
---|---|---|---|---|---|---|---|
1 | 15:00 | KEYNOTE: "Jerome Pearson Memorial Lecture" - Space Elevator Apex Anchor Initial Research | 20 | confirmed | Dr. Peter Swan | Space Elevator Development Corporation | United States |
2 | 15:20 | 10 | confirmed | Prof. Fumihiro Inoue | Shonan Institute of Technology | Japan | |
3 | 15:30 | 10 | confirmed | Ms. Momoe Terata | Shonan Institute of Technology | Japan | |
4 | 15:40 | 10 | confirmed | Dr. John Knapman | International Space Elevator Consortium | United Kingdom | |
5 | 15:50 | Technical issues and current development status for realizing a space elevator | 10 | confirmed | Dr. Yoji Ishikawa | Obayashi Corporation | Japan |
6 | 16:00 | The Space Elevator Apex Anchor : Functional Design Considerations and Parameter Effects | 10 | withdrawn | Mr. Peter Robinson | International Space Elevator Consortium | United Kingdom |
7 | 16:10 | Design considerations for a space manufacturing facility at the Apex Anchor | 10 | confirmed | Ms. Chi Lan Huynh | University of Houston | United States |
8 | 16:20 | Electromagnetic Coil Enhanced Space Elevators: Advancing Green Access to Space | 10 | confirmed | Ms. Flora Vyas | Vellore Institute of Technology | India |
9 | 16:30 | HEXAGONAL PRISM STRUCTURE FOR TETHER USED FOR SPACE ELEVATOR. | 10 | confirmed | Mr. Abhishek singh | National Space Society (USA) -Mumbai chapter | India |
10 | 16:40 | 10 | confirmed | Dr. Peter Swan | Space Elevator Development Corporation | United States | |
11 | 16:50 | 10 | Mr. Giorgio Gaviraghi | Unispace Exponential Creativity | Italy | ||
12 | 17:00 | 10 | confirmed | Mr. Ravan Akhundov | Azerbaijan State Oil and Industry University (ASOIU) | Azerbaijan |