The future of the space elevator

Similar documents
Cable Dragging Horizontal Takeoff Spacecraft Air Launch System

Energy. on this world and elsewhere. Instructor: Gordon D. Cates Office: Physics 106a, Phone: (434)

The Merit 1:48 scale Late War 80 ft. Elco PT Boat -By- T. Garth Connelly

Next Steps in Human Exploration: Cislunar Systems and Architectures

Travel: Detailed Flight Plan

ELECTRIC CURRENT. Name(s)

Rocket Races. Rocket Activity. Objective Students investigate Newton s third law of motion by designing and constructing rocketpowered

Energy. on this world and elsewhere. Instructor: Gordon D. Cates Office: Physics 106a, Phone: (434)

To determine which number of fins will enable the Viking Model Rocket to reach the highest altitude with the largest thrust (or fastest speed.

LUNAR INDUSTRIAL RESEARCH BASE. Yuzhnoye SDO proprietary

Unit 2: Lesson 2. Balloon Racers. This lab is broken up into two parts, first let's begin with a single stage balloon rocket:

time in seconds Amy leaves diving board

The Israeli revolution of the internal combustion engine

apply to all. space because it is an air-breather. Although from the atmosphere to burn its fuel. This limits

The GHOST of a Chance for SmallSat s (GH2 Orbital Space Transfer) Vehicle

Supersonic Combustion Experimental Investigation at T2 Hypersonic Shock Tunnel

Challenges of Designing the MarsNEXT Network

Rocket Activity Advanced High- Power Paper Rockets

A car-free world? Name:... Date:... Car-free Day comprehension. The Development of Cars

Part II. HISTORICAL AND ENGINEERING ANALYSIS OF AIRSHIP PLAN-AND- DESIGN AND SERVICE DECISIONS

Suitability of reusability for a Lunar re-supply system

FEDERAL SPACE AGENCY OF RUSSIAN FEDERATION LAVOCHKIN ASSOCIATION PROGRAM OF THE MOON EXPLORATION BY AUTOMATIC SPACE COMPLEXES

PNEUMATIC BIKES ABSTRACT

OF THE FUTURE-THE PNEUMATIC BIKE ECO FRIENDLY

IST Sounding Rocket Momo User Guide

Solar Electric Propulsion Benefits for NASA and On-Orbit Satellite Servicing

EXTENDED GAS GENERATOR CYCLE

Lunar Science and Infrastructure with the Future Lunar Lander

GK L A U N C H SER VICES MOSCOW 2017

External Aerodynamics: Lift of airship created only by buoyancy which doesn t need lift generating surface like an airfoil or a wing

Reducing Landing Distance

Deployment and Drop Test for Inflatable Aeroshell for Atmospheric Entry Capsule with using Large Scientific Balloon

Vector-R Forecasted Launch Service Guide

H-IIA Launch Vehicle Upgrade Development

Diagnostic. Enlightenment. The Path to

Nilar leads the way with high-voltage solutions for the electrical energy storage market

Martin J. L. Turner. Expedition Mars. Published in association with. Chichester, UK

MORE THAN PRESSURE SPRING RATE STAGGER CROSS WEIGHT CHANGES

Rocket 101. IPSL Space Policy & Law Course. Andrew Ratcliffe. Head of Launch Systems Chief Engineers Team

Name: Period: Due Date: Physics Project: Balloon Powered Car

AEROSPACE TEST OPERATIONS

Capabilities Summary and Approach to Rideshare for 20 th Annual Small Payload Rideshare Symposium NASA Ames Research Center June 12-14, 2018

Airships: A New Horizon for Science April 30 May 3, Worldwide Aeros Corp. Montebello, California. Presented by:

Electronic Testing Category 5

Electric Flight Potential and Limitations

THE KOREASAT5 PROGRAM

Before the Federal Aviation Administration Washington, D.C ) ) ) ) ) ) Formal Comments of Nickolaus E. Leggett

The distinguishing features of the ServoRam and its performance advantages

Barnett Spring Conversion for Liner

The All New 750cc Four

Transportation Copyright Council for Economic Education

SMARTSat. Shape Memory Alloy Research Technology Satellite. Allison Barnard Alicia Broederdorf. Texas A&M University Space Engineering Institute

A.M. MONDAY, 19 January minutes

Name: Space Exploration PBL

Adrestia. A mission for humanity, designed in Delft. Challenge the future

MAGNA DRIVETRAIN FORUM 2018

Europa Lander Mission Overview and Update

A Space Solar Power Industry for $2 Billion or Your Money Back

THE FALCON I LAUNCH VEHICLE Making Access to Space More Affordable, Reliable and Pleasant

Automotive Research and Consultancy WHITE PAPER

iss Field of search , 31. Primary Examiner J. Woodrow Eldred

Robots from Junk. Vocabulary autonomous, center of mass, lander, robotics, rover

Application Of Belt Winder For Conveyor Replacements In Coal Handling Plants Of Thermal Power Stations

Heat Shield Design Project

What do we Know? Concepts

Battery Pack & Electrical Examples. What other teams saw that you don t need to see Steve McMullen

ELECTRIC PROPULSION MISSION TO GEO USING SOYUZ/FREGAT LAUNCH VEHICLE M.S. Konstantinov *, G.G. Fedotov *, V.G. Petukhov ±, G.A.

ASTRIUM. Lunar Lander Concept for LIFE. Hansjürgen Günther TOB 11. Bremen, 23/

INDIAN INSTITUTE OF TECHNOLOGY KHARAGPUR NPTEL ONLINE CERTIFICATION COURSE. On Industrial Automation and Control

EPIC Workshop 2017 SES Perspective on Electric Propulsion

Table of Contents. Executive Summary...4. Introduction Integrated System...6. Mobile Platform...7. Actuation...8. Sensors...9. Behaviors...

Air Brakes From Real Trains

MagneMotion Maglev Demonstration on ODU Guideway

Massachusetts Space Grant Consortium

Generation revolution.

Creating Innovation Conducive to Energy and the Environment By Takeshi Uchiyamada Chairman of Toyota Motor Corporation

SSC Swedish Space Corporation

Preliminary Cost Analysis MARYLAND

Mars Surface Mobility Proposal

Unit 1 Introduction to VEX and Robotics

Development of Low-thrust Thruster with World's Highest Performance Contributing to Life Extension of Artificial Satellites

CHAPTER 6.3: CURRENT ELECTRICITY

EPIC Gap analysis and results

Porting Applications to the Grid

About Steel Market Development Institute

Solar Panel with Mechanical Tracking

NASA s Choice to Resupply the Space Station

On Orbit Refueling: Supporting a Robust Cislunar Space Economy

Good afternoon. We're going to be talking today about frontiers of imagination in space exploration

FROM BRAIN WAVE TO HEAVY LIFT TERMINAL IN ONE YEAR

Everything Leading Up to Nuclear Cars. next 150 years is to have a car that runs on the splitting of atoms. This will be a clean and

Objectives: I can convert units using conversion factors in the same system. I can convert units using conversion factors between systems.

TEMPERATURE EFFECTS ON THE DAMPER

Transportation Options for SSP

Systems Engineering. Chris Hall AOE 4065 Fall 2005

The European Lunar Lander Mission

Design and Analysis of Stirling Engines. Justin Denno Advised by Dr. Raouf Selim

Thinking Outside the Cube

Deployment and Flight Test of Inflatable Membrane Aeroshell using Large Scientific Balloon

INVENTION DISCLOSURE MECHANICAL SUBJECT MATTER EFFICIENCY ENHANCEMENT OF A NEW TWO-MOTOR HYBRID SYSTEM

Transcription:

1 The future of the space elevator JOSÉ GERARDO CHÁVEZ ROSAS gerardochav@yahoo.com.mx http://aemex.orgfree.com/ Introduction The Space Elevator is the most promising Space Transportation system on the drawing boards today, combining scalability, low cost, qualify of ride, and safety to deliver truly commercial-grade space access - practically comparable to a train ride to space. Rocket-based space launch systems are inherently limited by the physics of rocket propulsion. More than 90% of the rocket's weight is propellant, and the rest is split between the weight of the fuel tank and the payload. It is very difficult (if not impossible) to make such a vehicle safe or low cost. A target cost of $1000 per kg is proving to be impossible to reach. In comparison, airliners charge us about $1 per pound, and train transportation is in cents per pound. The Space Elevator is based on a thin vertical tether stretched from the ground to a mass far out in space, and electric vehicles (climbers) that drive up and down the tether. The rotation of the Earth keeps the tether taut and capable of supporting the climbers. The climbers travel at speeds comparable to a fast train, and carry no fuel on board - they are powered by a combination of sunlight and laser light projected from the ground. While the trip to space takes several days, climbers are launched once per day. The first "baseline" design will use 20 ton climbers, but by making the tether thicker (which can be done using the Space Elevator itself) we can grow the Space Elevator to lift 100, or even 1000 tons at a time. In addition to launching payloads into orbit, the Space Elevator can also use its rotational motion to inject them into planetary transfer orbits - thus able to launch payloads to Mars, for example, once per day. Imagine the kind of infrastructure we can set up there, waiting for the first settlers to arrive... Looking back from the year 2100, the construction of the Space Elevator will be considered to mark the true beginning of the Space Age, much like the advent of the airplane or steamboat heralded the true commercial use of the air and sea. The above is taken from an ISEC (International Space Elevator Consortium) document which explains the basics of the current draft of the space elevator. The document states that the projects are based on a vertical tether stretched thin from the ground to a mass far out in space, and electric vehicles (climbers) that drive up and down the tether. The rotation of the Earth keeps the tether taut and capable of supporting the climbers. The climbers are powered by a combination of sunlight and laser light projected from the ground. However, my proposals do not incorporate laser beams, although two of my projects are based on photocells. I think that, in practice, laser beams may not have sufficient capacity to carry a heavy load (100 or 1000 tons.); even photocells do not have that power conversion capacity. It is for this reason that my proposals are not based on laser beams but on existing techniques we use every day. Below are my proposals for an alternative space elevator. I believe that in all cases they could be used alone or in combination with my other proposals for the best performance of the space elevator. The challenge is not easy but I think it's absolutely possible! Clarification: In all cases, I present a very simple design for the cabin of the elevator, without radiation protection. This is for reasons of illustration; obviously there must be modifications in the real projects.

2 Project 1: Space elevator with chain of nanotubes and space electric motors Explanation: in this project we need only solar panels placed in geostationary orbit large enough to lift the desired weight and electric motors that will raise either a chain or a tether made of nanotubes. The electric motor powered by photocells would be situated close to the photocells. The chains or tethers may have a counterweight at the other end similar to that used in building elevators to enhance the efficiency of its operation. A second elevator could even be used as a counterweight so as one moves up the other goes down.

3 Project 2: Space elevator with helium balloons and photocells Explanation: to raise the platform, along with the cabin and solar panels, liquid helium is released from a tank which serves at the same time as a support base and lifting platform for the cabin and solar panels. Balloons are filled with helium gas and these balloons will raise the platform the first 50 km into space. The cabin is independent of the base so, after reaching the height of 50 km, the photocells will begin to provide the necessary power to the electric motors allowing the cabin to continue its trip into space, driving up the tether. To lower the cabin from space the cabin is left to fall down the tether in controlled fashion until reaching 50 km altitude where the platform is waiting with helium balloons. The compressors begin their work to get gaseous helium back into the tank (by making it liquid) and the whole device continues its descent to the earth. Perhaps this is the most complicated of my proposals, but the idea is to use the height provided by the balloons to improve the efficiency of the photocells as the radiation is greater at that altitude (50 km).

4 Project 3: Space elevator with low speed rocket or power The basic idea is this: To get into orbit a spacecraft needs to develop a very high speed in a very short time. In this case that huge speed is not necessary as the cabin cannot fall because it is supported by or hung from the tether or cables of nanotubes. Therefore, a low speed rocket (which represents a huge saving of fuel, weight and size) will be able to put into "orbit" the cabin or anything else at a very low cost. To get down de cabin to earth, the rocket is put upside down.

5 Project 4: Space elevator with electric conductive cables or tether of nanotubes The basic idea is this: Can electrically conductive nanotubes be manufactured? If so, then nanotubes could not only support the cabin but could also feed the lifting system of electric motors and the problem would be solved. That is to say: an electrically conductive cable made of nanotubes could serve the same way we use cables in a trolley but also serving as a support at the same time.

6 Project 5: Endless belt space elevator The main idea of this project is to use a lifting endless belt to raise the space elevator from the ground with the help of a pulley and using a large electric motor (as many as required) here on earth. The elevator would be attached to the lifting endless belt or tether made of nanotubes. The pulley would be located at the desired height, perhaps 300 kilometers or more. The chains or tethers may have a counterweight at the other end as we use in building elevators to enhance the efficiency of its operation. You could even use a second elevator as a counterweight so as one moves up the other goes down, as in my project number 1. The great advantage of this proposal is that all the energy is provided from the earth and the cabin only carries the payload or passengers into space which represents a huge energy savings. This technology is very simple and practical. It is in fact the one which I consider the most practicable.

7 CONCLUSIONS Hello, my name is Gerardo Chavez, I am a 58 year old Mexican inventor and I'm very happy to collaborate on this fantastic project. At first I thought it would be impossible to develop the proposed space elevator, but then I realized that it was not only possible but practicable in a few years with the technology we have today. The results of these ideas are five projects that I present to you today. Using the techniques I propose the only problem would be in the construction and positioning of the cable, rope, tether, band, etc. made of nanotubes and the launching of the geostationary satellite. The other needed devices are made with today's technologies. I think it's definitely possible to build a space elevator in the short term. On the other hand I think that in this particular case the laser beam system is not the best option because if we want to put into orbit 100 or 10000 tones imagine the size of the laser beam to perform this task. That is why my proposals are conventional techniques currently used and much more powerful. Thank you very much for your attention and I hope some of these proposals contribute to the realization of the space elevator. 1. Introduction 1 2. The development-process of the Climber 2 3. Conclusions 7 With the kind support of ICYT (Institute of Science and Technology) of Mexico City and Jorge Ramirez Thanks also to Brian Kelly José Gerardo Chávez Rosas México D.F. México Email: gerardochav@yahoo.com.mx Web site: http://aemex.orgfree.com/ Tel: + 52 (55) 28 73 06 85