A Private Commercial Space Company EA02P046V5

Similar documents
Cygnus Payload Accommodations: Supporting ISS Utilization

Antares Rocket Launch recorded on 44 1 Beyond HD DDR recorders Controlled by 61 1 Beyond Systems total

ENERGIA 1. IDENTIFICATION. 1.1 Name. 1.2 Classification Family : K Series : K-1/SL-17 Version : 4 strap-ons

Next Steps in Human Exploration: Cislunar Systems and Architectures

Wernher von Braun Symposium. Dream Chaser Program. Sierra Nevada Corporation. Overview. October For the

Copyright 2016 Boeing. All rights reserved.

Boeing CST-100. Commercial Crew Transportation System. Keith Reiley, The Boeing Company. February, 2011

Notes: GENERAL DYNAMICS EARLY LUNAR ACCESS [1993]

MARS-OZ: A Design for a Simulated Mars Base in the Arkaroola Region

GK L A U N C H SER VICES MOSCOW 2017

NASA s Choice to Resupply the Space Station

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

Taurus II. Development Status of a Medium-Class Launch Vehicle for ISS Cargo and Satellite Delivery

SPACE LAUNCH SYSTEM (SLS)

Routine Scheduled Space Access For Secondary Payloads

r bulletin 96 november 1998 Figure 1. Overall ATV configuration (ESA/D. Ducros)

Massachusetts Space Grant Consortium

UNCLASSIFIED R-1 ITEM NOMENCLATURE

Instruction Manual: Space Launch System Payload Transfer Module (PTM)

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

NASA Glenn Research Center Intelligent Power System Control Development for Deep Space Exploration

SABRE FOR HYPERSONIC & SPACE ACCESS PLATFORMS

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

The Role of Electric Propulsion in a Flexible Architecture for Space Exploration

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

Building Bridges for Lunar Commerce

From MARS To MOON. V. Giorgio Director of Italian Programs. Sorrento, October, All rights reserved, 2007, Thales Alenia Space

UNCLASSIFIED. FY 2016 Base FY 2016 OCO

Blue Origin Achievements and plans for the future

WHAT WE WILL DISCUSS IN THIS VIDEO

AN OPTIMIZED PROPULSION SYSTEM FOR Soyuz/ST

Space Architecture. Master s Thesis Project Jain, Abhishek Dec. 2 nd, 2013

The DoD Space Test Program Standard Interface Vehicle (ESPA) Class Program

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

The ATV Programme "Jules Verne"

ARCHIVED REPORT. For data and forecasts on current programs please visit or call

QinetiQ Electric Propulsion

IAC-04-IAF-S.2.06 NEW PROPELLANT IGNITION SYSTEM IN LV SOYUZ ROCKET ENGINE CHAMBERS

Atlas V Launches the Orbital Test Vehicle-1 Mission Overview. Atlas V 501 Cape Canaveral Air Force Station, FL Space Launch Complex 41

Private Development of a Low-Cost, Lightweight Launch-Reentry Pressure Suit

CHAPTER 1 INTRODUCTION

A LEO Propellant Depot System Concept for Outgoing Exploration

SPACE STATIONS USING THE SKYLON LAUNCH SYSTEM

Baseline Concepts of the Kayser-Threde Team

THE 21 ST CENTURY SPACE SHUTTLE

ULA's new Vulcan rocket 24 June 2015, by Ken Kremer, Universe Today

BIMODAL NUCLEAR THERMAL ROCKET (BNTR) PROPULSION FOR FUTURE HUMAN MARS EXPLORATION MISSIONS

BIMODAL NUCLEAR THERMAL ROCKET (BNTR) PROPULSION FOR FUTURE HUMAN MARS EXPLORATION MISSIONS

Rocket Activity Advanced High- Power Paper Rockets

Development of Japan s Next Flagship Launch Vehicle

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

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

Space Exploration Via Technology Demonstration and Small Satellite Missions Flown on Reusable Launch Vehicles SSC04-X-8.

UK Continental Shelf (UKCS) Oil and Gas Production and the UK Economy. Mike Earp

RDT&E BUDGET ITEM JUSTIFICATION SHEET (R-2 Exhibit) June 2001

SPACE LAUNCH SYSTEM. Steve Creech Manager Spacecraft/Payload Integration & Evolution August 29, 2017 A NEW CAPABILITY FOR DISCOVERY

As the global energy sector

MS1-A Military Spaceplane System and Space Maneuver Vehicle. Lt Col Ken Verderame Air Force Research Laboratory 27 October 1999

Pre-Launch Procedures

Suitability of reusability for a Lunar re-supply system

EPIC Workshop 2017 SES Perspective on Electric Propulsion

HARAS High Availability Redundant Actuation Systems

European Lunar Lander: System Engineering Approach

The Intermediate Outpost - An Alternate Concept for Human Lunar Exploration

ACAS X Next Generation Collision Avoidance

Lunar Cargo Capability with VASIMR Propulsion

Cal Poly CubeSat Workshop 2014

Propulsion Controls and Diagnostics Research at NASA GRC Status Report

Exploration Architecture Update

Analysis of Power Storage Media for the Exploration of the Moon

NASA s Space Launch System Marks Critical Design Review

Space Exploration Via Technology Demonstration and Small Satellite Missions Flown on Reusable Launch Vehicles

AMSAT-NA FOX Satellite Program

Leading the Way to Electric Propulsion in Belfast

OMOTENASHI. (Outstanding MOon exploration TEchnologies demonstrated by NAno Semi-Hard Impactor)

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

The Common Spacecraft Bus and Lunar Commercialization

Program update February, 2017

Impact of Technology on Fuel Efficiency

Electric propulsion as game changer for CubeSat: mission analysis with LOTOS

Case Study: ParaShield

Advancing the TWV Fleet 10 May 2016

Update on Progress of SSIKLOPS (Space Station Integrated Kinetic Launcher for Orbital Payload Systems) - Cyclops

AMBR* Engine for Science Missions

Moon Express Summary. Dr. Andrew Aldrin President, Moon Express, Inc. 12 June, Science Network. Sample Return ME-1: GLXP

USGIF Small Satellite Working Group Resilient SmallSat Launch-on-Demand

ORBITAL EXPRESS Space Operations Architecture Program 17 th Annual AIAA/USU Conference on Small Satellites August 12, 2003

Formation Flying Experiments on the Orion-Emerald Mission. Introduction

Creating a zero-emissions shipping world

UNCLASSIFIED R-1 ITEM NOMENCLATURE. FY 2014 FY 2014 OCO ## Total FY 2015 FY 2016 FY 2017 FY 2018

In-Space Demonstration of HighPerformance Green Propulsion (HPGP) and its Impact on Small Satellites

July Turbomeca Safety Initiatives

Future NASA Power Technologies for Space and Aero Propulsion Applications. Presented to. Workshop on Reforming Electrical Energy Systems Curriculum

Affordable Human Moon and Mars Exploration through Hardware Commonality

Rotor Sail Solution. Tuomas Riski - Norsepower Steen Jacobsen - Maersk Tankers Energy Technologies Institute LLP - Subject to notes on page 1

NEXT Exploration Science and Technology Mission. Relevance for Lunar Exploration

UNCLASSIFIED FY 2017 OCO. FY 2017 Base

Results of the Airbus DS led e.deorbit Phase B1 ESA study. Dr.-Ing. Stéphane Estable ESA Clean Space Industrial Days, October 2017

Analysis of Launch and Earth Departure Architectures for Near-Term Human Mars Missions

Lunar Surface Access from Earth-Moon L1/L2 A novel lander design and study of alternative solutions

Transcription:

A Private Commercial Space Company

Outline Who We Are The Technology The Next Step

Excalibur Almaz was formed to revolutionize the spaceflight industry through regular manned and unmanned flights to orbit Excalibur Almaz is positioning itself to become the first private F company to offer routine orbital spaceflights Excalibur Almaz is a private, international space exploration company formed in 2005 The company was created to provide routine, affordable access to and from space for customers around the globe Using updated and modernized proven Russian legacy space systems and other state of the art technology, EA will offer transportation for purposes of exploration, research, and science 3

EA consists of top executives in the aerospace, business and financial industries Executive Profiles Art Dula CEO & Founder 30+ years as an attorney specializing in aerospace Founder of Spacehab, Inc. Director and President of Space Commerce Corporation ISU board member Valery Tokarev Cosmonaut Consultant 20+ years in aerospace Commander of the Soyuz and ISS Two Spaceflight Mission totaling 200+ days in space J. Buckner Hightower Executive Vice President Worked in Soviet Union and Russian Federation since 1988 25+ years of experience in capital formation and financial consulting ISU board member Vladimir Titov General Director Russia Record setting 387 days in space Trained on the Almaz capsule Former Director of Space and Communications for the Boeing Company in Russia

EA s global reach offers widespread access to key customers and partners enabling stream-lined operations Excalibur Almaz Ltd. Isle of Man, UK Excalibur Almaz USA Houston, TX Excalibur Almaz USA Tallahassee, FL Excalibur KK Tokyo, Japan Space Estafetta Moscow, Russia 5

Outline Who We Are The Technology The Next Step

The EA Space System elements are a mixture of proven and state of the art technology Reusable Re-entry Vehicle (Orbital Configuration) Service Module (Tourist Configuration) Service Module (Cargo Configuration) 7

The Almaz Spacecraft Developed by NPO Machinostroyenia Program has flown 10 times (3 reentry vehicle reuses) NPOM assessments indicate multiple reuse capability EA currently owns 4 reentry vehicles 8

Almaz Reentry Vehicle Tourist Configuration Crew Size: 3 On-orbit Mass Estimate: ~4 metric tonnes (without escape system) Designed for assured safe reentry proven on multiple space flights and extensive ground testing Currently the only reusable spacecraft in existence besides the U.S. space shuttle 9

Service Module Tourist Version 14.2m 9.9m Planned duration onorbit ~ 5 days Mass target 2 Metric Tonnes Design goal to use an existing launch vehicle adaptor 10

Service Module Tourist Version 11

Service Module Cargo Concept Planned duration onorbit ~5 days maximum free flight, up to one month attached to a Space Station Mass target 3-4 Metric Tonnes dependent on Cargo load Design goal to use an existing launch vehicle adaptor 12

Service Module Cargo Concept Original Almaz System (shown in on-orbit configuration prior to dock to the Salyut Space Station) Capsule System Service/Habitation Module Equivalent (Included propulsion) Cargo Concept Legacy Capsule System (delete crew provisions and escape tower, update avionics, add simple ECLSS and Passive Common Berthing Mechanism) Service Module with Propulsion/Attitude Control The system proposed is a de-evolution of the original Almaz TKS system. Provisions for crew are removed, ECLSS simplified, state of the art Avionics, propulsion/attitude control and rendezvous system based on proven technology 13

Outline Who We Are The Technology The Next Step

Schedule and Timeline Goals Manned Test Flight Excalibur Almaz Founded First Revenue Flight Preparation and modernization 2005 2010 2011 2012 2013 2014 2015 Unmanned Test Flight Excalibur Almaz, LTD Proprietary Data