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CYCLICAL VISITS TO MARS VIA 
ASTRONAUT HOTELS 
Presentation to the 
NASA Institute for Advanced Concepts (NIAC) 
3rd Annual Meeting: 
Visions of the Future in Aeronautics and Space 
by 
Kerry T. Nock 
Global Aerospace Corporation 
http://www.gaerospace.com 
June 5-6, 2001 
Global 
Aerospace Corporation
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation PHASE I STUDY CONTRIBUTORS 
Global Aerospace Corporation (GAC) 
Dr. Kim M. Aaron 
Dale R. Burger 
Dr. Angus D. McRonald 
Kerry T. Nock, Principal Investigator and NIAC Fellow 
Susan L. Nock 
Brenda Wistor-Linfield 
Science Applications International Corporation (SAIC) 
Alan L. Friedlander 
Mark K. Jacobs 
Jerry A. Rauwolf 
Planetary Resource Utilization Consultant 
Dr. Michael B. Duke 
Solar Electric Propulsion Technical Advisor 
Dr. John R. Brophy, Jet Propulsion Laboratory 
Global Aerospace Corporation 3 KTN - NIAC Annual Meeting - June 5, 2001
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation TOPICS 
INTRODUCTION 
ORBIT ANALYSIS 
TRANSPORTATION SYSTEM ARCHITECTURE 
SYSTEM MODELING, ANALYSIS & COSTS 
SIGNIFICANCE TO NASA 
SUMMARY 
Global Aerospace Corporation 4 KTN - NIAC Annual Meeting - June 5, 2001
INTRODUCTION
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation BACKGROUND 
• 1985 National Commission on Space (NCOS) 
– Mars transportation infrastructure for permanent Mars base 
– Use of cyclic orbits 
– Cycling vehicles (CASTLES), spaceports and taxis 
• Revolutionary NIAC concept being studied by Global Aerospace 
– Reduce crew occupation to only 5 months 
– Increase systems autonomy 
– Eliminate artificial gravity from cycling vehicles 
– Reduce cycling vehicle size 
– Use solar energy for surface and space power systems 
– Employ solar-powered ion propulsion systems (IPS) throughout 
– Significantly reduce reliance on earth propellants, consumables and 
refurbishment, repair and upgrade (RRU) cargo 
Global Aerospace Corporation 6 KTN - NIAC Annual Meeting - June 5, 2001
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation CONCEPT MOTIVATION 
• Create permanent elements of a Mars transportation system 
• Take advantage of natural orbital physics to facilitate Mars 
transportation 
• Eliminate need for new, expensive class of rockets and launchers 
• Offer environmentally safe technology, without political baggage, 
for transportation to and from mars 
• Increase reliance on in situ resources for Mars transportation 
architecture 
• Accelerate the timeframe for permanent inhabitation of Mars 
Global Aerospace Corporation 7 KTN - NIAC Annual Meeting - June 5, 2001
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation KEYS TO THE CURRENT CONCEPT 
• Cycler orbits between Earth and Mars that enable fast, frequent 
transfers between these planets 
• Astronaut hotels, or Astrotels, which are small transport 
vehicles capable of carrying 10 people on cycling orbits between 
planets 
• Orbital spaceports at the planets and very small, fast, 
hyperbolic transfer vehicles, or taxis, between spaceports and 
astrotels. 
• Propellant and life support in situ resource manufacturing 
plants 
• Cargo vehicles that utilize low-energy, long-flighttime orbits to 
transport propellant and low value cargo to and from planets 
• Shuttles to and from spaceports and planetary surfaces 
Global Aerospace Corporation 8 KTN - NIAC Annual Meeting - June 5, 2001
ORBIT ANALYSIS
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation ALDRIN CYCLERS 
Global Aerospace Corporation 10 KTN - NIAC Annual Meeting - June 5, 2001
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation EXAMPLE ALDRIN 
UP-CYCLER SEQUENCE 
E3 E1 
M2 
M4 
Global Aerospace Corporation 11 KTN - NIAC Annual Meeting - June 5, 2001
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation UP-CYCLER LOW THRUST 
TRAJECTORY SHAPING 
Thrusting Phase 
Coast Phase 
• 2nd Correction of Up Orbit 
• Thrust Period 430 days 
• Coast Period 350 days 
• Uncrewed During Thrusting 
Global Aerospace Corporation 12 KTN - NIAC Annual Meeting - June 5, 2001
TRANSPORTATION SYSTEM 
ARCHITECTURE
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation TRANSPORTATION ARCHITECTURE 
Global Aerospace Corporation 14 KTN - NIAC Annual Meeting - June 5, 2001
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation DOWN-CYCLER 
PLANETARY GEOMETRY 
Phobos 
Mars 
Mars 
Spaceport 
Taxi 
Aldrin Down Cycler 
Mission Profile 
Astrotel 
Aldrin Down 
Cycler 
Trajectory 
Propulsive Delta-Vs 
L1 Earth 
Spaceport 
Taxi 
Moon 
Aerocapture 
Maneuver Earth 
Global Aerospace Corporation 15 KTN - NIAC Annual Meeting - June 5, 2001
ASTROTEL CONCEPT 
Xenon 
Propellant 
Tank 
Ion Engines 
(Eight, 50 cm, 
17 kW, 5000s) 
Hab Module 
Cargo Pod 
Solar Array 
(160 kW) 
Astrotel Mass: 69.1 mt 
Eva
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation ION PROPULSION SYSTEM (IPS) 
Global Aerospace Corporation 17 KTN - NIAC Annual Meeting - June 5, 2001
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation EXAMPLE AERO-ASSIST 
PROFILE AT MARS 
Entry Interface 125 km 
Begin Aero-Cruise 
Pitch Over to Lmax Pitch Back to L=0 
Scale Exaggerated 
Mars 
40-50 km 
Altitude 
Entry 
L=0 
In 
Orbit 
Global Aerospace Corporation 18 KTN - NIAC Annual Meeting - June 5, 2001
ISS TRANSHAB CONCEPT 
(Courtesy NASA/JSC) 
Modifications 
• Expansion of crew from 6 to 10 
• 6-times volume/crew as STS 
• Expansion of radiation protection 
• Added docking port 
• Include Astrotel command and 
control systems
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation TAXI CONCEPT: 
Crew Module LEAVING EARTH SPACEPORT 
Aeroshell (Elliptical 
Raked Cone) 
Propellant Tanks 
Rocket Engines 
(Extended Nozzle) 
Taxi Dry Mass: 19.1 mt 
Global Aerospace Corporation 20 KTN - NIAC Annual Meeting - June 5, 2001
TAXI CREW MODULE 
Crew Space Equal to Apollo 
Docking Port 
Variable 
g-Vector 
Seats (10) 
SEAT ROTATION
TAXII IIN AEROCRUIISE OVER MARS
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation IN SITU RESOURCE 
UTILIZATION STRATEGIES • Moon --> Polar Ice 
– Excavate regolith, heat and extract water (10.2 kg/hr) 
– Electrolyze some water into O2/H2 and liquefy to LOX/LH for lunar water tanker 
– Liquefy and transport most water to earth spaceport 
• Earth Spaceport --> ~100% Sun 
– Electrolyze Lunar water Into O2/H2 and liquefy to LOX/LH (1.6 kg/hr) 
– LOX/LH storage for Taxi 
• Phobos --> O2-Bearing Regolith 
– Carbon reduction of regolith to produce O2 (23.2 kg/hr) 
– Liquefy to LOX and transport to Mars spaceport for storage 
• Mars Spaceport --> ~100% Sun 
– LOX/LH storage for Taxi 
• Mars Surface --> Water-Bearing Regolith 
– Excavate regolith (dunes), heat and extract water (8.1 kg/hr) 
– Electrolyze water into O2/H2 and liquefy to LOX/LH for Mars shuttle 
Global Aerospace Corporation 23 KTN - NIAC Annual Meeting - June 5, 2001
SYSTEM MODELING, ANALYSIS 
AND COSTS
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation MAMA 
Astrotels 
- Type 1 
- Type 2 
- Type n 
SYSTEM INTEGRATOR 
INPUTS OUTPUTS* ELEMENT INTERFACES 
Orbital 
Nodes 
- Type 1 
- Type 2 
- Type n 
Surface 
Facilities 
- Type 1 
- Type 2 
- Type n 
Ground 
Facilities 
(Earth) 
- Type 1 
- Type 2 
- Type n 
ISRU 
Systems 
- Type 1 
- Type 2 
- Type n 
Launch 
Systems 
- Type 1 
- Type 2 
- Type n 
Transfer & 
Excursion 
Vehicles 
- Type 1 
- Type 2 
- Type n 
Launch 
Vehicles 
Trajectory 
Analyses 
Propulsion 
Systems 
Power 
Systems 
Life Support 
Systems 
Other 
Systems 
* System Integrator Output includes a standard WBS-format for all architecture candidates 
ELEMENTS 
SUPPORT 
ANALYSES 
Global Aerospace Corporation 25 KTN - NIAC Annual Meeting - June 5, 2001
EXAMPLE MAMA SYSTEM ELEMENT
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation CARGO USE PROFILE SUMMARY 
Location-------------> At LEO At Earth 
Spaceport 
At Mars 
Spaceport 
At Surface 
of Mars 
At Surface 
of Moon 
At Astrotels 
(2 vehicles) 
Total Cargo Requirements 
LOX 122,631 1,036,348 282,339 
LH 17,519 148,050 40,334 
Water 157,669 363,007 
Xenon 245,106 5,751 
Refurb Mass 149,863 37,800 80,259 54,061 5 6 7 14,692 
Augmentation Tanks 107,827 107,827 
Crew Consumables 1 1 9 , 1 4 0 1 1 9 , 1 4 0 
Communications Satellites 
Total Mass Required 621,935 335,619 1,372,483 739,741 5 6 7 139,583 
• Cargo requirements over 15-years 
• All masses in kg 
Global Aerospace Corporation 27 KTN - NIAC Annual Meeting - June 5, 2001
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation CARGO DELIVERY SYSTEMS 
REQUIREMENTS SUMMARY 
Location-------------> At LEO At Earth 
Spaceport 
Delivery Systems 
SEP Freighter Delivered Cargo 37,800 336,135 139,583 
Cargo Freighter Each Trip 5,400 48,019 19,940 
Lunar Water Tanker Total 157,669 5 6 7 
Lunar Water Tanker Each Trip 22,524 81 
Phobos LOX Tanker Total 1,036,348 
Phobos LOX Tanker Each Trip 34,545 
Mars Shuttle 54,061 
Mars Shuttle Each Trip 7,723 
All masses in kg 
At Mars 
Spaceport 
At Surface 
of Mars 
At Surface 
of Moon 
At Astrotels 
(2 vehicles) 
Global Aerospace Corporation 28 KTN - NIAC Annual Meeting - June 5, 2001
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation NIAC / NCOS COMPARISON 
Item NCOS 
Study 
NIAC 
Study 
Factor 
Cyclic Transport Vehicle 
Size, mt 
460 70 7 
Total 15-year 
Propellant and 
Consumables, mt 
34,335 2,011 17 
Lunar LOX Production 
Rate, kg/day 
4,014 73 55 
Phobos LOX Production 
Rate, kg/day 
1066 189 6 
Primary Power 
Generation Mode 
Nuclear Solar -- 
Global Aerospace Corporation 29 KTN - NIAC Annual Meeting - June 5, 2001
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation KEY COST ASSUMPTIONS 
• FY 2000 dollars 
• Full cost accounting on all life cycle elements 
• Major cost elements include: 
– Advanced Technology Development 
– Flight System Development 
– Launch (specific launch vehicle cost of $2000/kg) 
– Operations (15 years, includes RRU & propellants/consumables) 
Global Aerospace Corporation 30 KTN - NIAC Annual Meeting - June 5, 2001
Global 
Aerospace Corporation SYSTEM INTEGRATOR OUTPUT: 
Cyclical Visits To Mars via Astronaut Hotels 
Global Aerospace Corporation 31 KTN - NIAC Annual Meeting - June 5, 2001 
8,000 
RECURRING COSTS 
0 
1,000 
2,000 
3,000 
4,000 
5,000 
6,000 
7,000 
Astrotel 
Escape Pod 
Earth Spaceport 
Mars Spaceport 
Taxi 
Mars Cargo Freighter 
Astrotel Cargo 
Freighter 
LEO Shuttle 
Lunar Water Tanker 
Mars Shuttle 
Phobos LOX Tanker 
Mars Base 
Lunar Base 
Lunar Water Mine 
L1 Electr & Storage 
Phobos LOX Plant 
Mars Surf Water 
Plant 
Mars Spaceport 
Storage 
$M
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation SYSTEM INTEGRATOR OUTPUT: 
LIFE CYCLE (15 YEARS) COSTS 
30,000 
25,000 
20,000 
15,000 
10,000 
5,000 
0 
AdvTech DEVELOPMENT & LAUNCH OPERATIONS 
Adv Tech Dev 
Adv Tech Testing 
Flight System Design 
Flight Subsys Fab 
System Assy, Integ, 
Test 
LV Ground Facility 
Proc 
Launch & Checkout 
Orbital Assy, I&T 
Startup Ops 
SS Ops 
Refurbishment 
Hardware 
Disposal 
$M 
4.0 Operations 
3.0 Launch 
Services 
2.0 Flight 
System Dev 
1.0 Advanced 
Technology Dev 
Global Aerospace Corporation 32 KTN - NIAC Annual Meeting - June 5, 2001
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation SUMMARY OF 
COST ESTIMATES 
Development ~$50B* 
Operations ~$40B† 
Total Lifecycle ~$90B¥ 
____________________ 
* - ~$5B/yr for 10 years 
† - ~$3B/yr for 15 years 
¥ - For reference, the “90-day Study” (1989) costs for human exploration to the 
Moon and Mars was estimated at ~$400B and the NASA Mars Reference 
Mission (1997) was estimated at ~$40B. 
Global Aerospace Corporation 33 KTN - NIAC Annual Meeting - June 5, 2001
SIGNIFICANCE OF CONCEPT TO NASA
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation 
SIGNIFICANCE TO NASA 
• Facilitates human exploration to Mars and beyond 
• Assists the expansion of scientific knowledge by providing 
ready access to Mars by scientists 
• Provides safe, frequent and affordable access to Mars 
• Creates a significant element of the transportation 
architecture thus contributing to the establishment of a 
permanent human presence on Mars 
Global Aerospace Corporation 35 KTN - NIAC Annual Meeting - June 5, 2001
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation PHASE II 
• Key Team Members 
– GAC 
– SAIC - MAMA development & costing, orbit analysis 
– Purdue (Dr. Longuski) - Orbit analysis 
– Colorado School of Mines (Dr. King) - ISRU Concepts 
– Dr. Michael Duke - ISRU 
• Key Technical Tasks 
– Cyclic orbit concepts and research 
– Advanced aero-assist concepts 
– ISRU system concepts development 
– Develop and assess transportation options 
– MAMA development and costing 
Global Aerospace Corporation 36 KTN - NIAC Annual Meeting - June 5, 2001
SUMMARY
Cyclical Visits To Mars via Astronaut Hotels 
Global 
Aerospace Corporation SUMMARY 
• This transportation architecture, along with Astrotels, enable 
low-cost, frequent access to Mars for scientists and explorers 
• System concepts have been developed that could be utilized in 
expedition phases of Mars exploration 
• This architecture provides a framework and context for future 
technology advance and robotic exploration 
• The tools developed during this study can be used to analyze 
and compare future technology and system options 
Global Aerospace Corporation 38 KTN - NIAC Annual Meeting - June 5, 2001
Astronaut hotelsjun01

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Astronaut hotelsjun01

  • 1. CYCLICAL VISITS TO MARS VIA ASTRONAUT HOTELS Presentation to the NASA Institute for Advanced Concepts (NIAC) 3rd Annual Meeting: Visions of the Future in Aeronautics and Space by Kerry T. Nock Global Aerospace Corporation http://www.gaerospace.com June 5-6, 2001 Global Aerospace Corporation
  • 2. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation PHASE I STUDY CONTRIBUTORS Global Aerospace Corporation (GAC) Dr. Kim M. Aaron Dale R. Burger Dr. Angus D. McRonald Kerry T. Nock, Principal Investigator and NIAC Fellow Susan L. Nock Brenda Wistor-Linfield Science Applications International Corporation (SAIC) Alan L. Friedlander Mark K. Jacobs Jerry A. Rauwolf Planetary Resource Utilization Consultant Dr. Michael B. Duke Solar Electric Propulsion Technical Advisor Dr. John R. Brophy, Jet Propulsion Laboratory Global Aerospace Corporation 3 KTN - NIAC Annual Meeting - June 5, 2001
  • 3. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation TOPICS INTRODUCTION ORBIT ANALYSIS TRANSPORTATION SYSTEM ARCHITECTURE SYSTEM MODELING, ANALYSIS & COSTS SIGNIFICANCE TO NASA SUMMARY Global Aerospace Corporation 4 KTN - NIAC Annual Meeting - June 5, 2001
  • 5. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation BACKGROUND • 1985 National Commission on Space (NCOS) – Mars transportation infrastructure for permanent Mars base – Use of cyclic orbits – Cycling vehicles (CASTLES), spaceports and taxis • Revolutionary NIAC concept being studied by Global Aerospace – Reduce crew occupation to only 5 months – Increase systems autonomy – Eliminate artificial gravity from cycling vehicles – Reduce cycling vehicle size – Use solar energy for surface and space power systems – Employ solar-powered ion propulsion systems (IPS) throughout – Significantly reduce reliance on earth propellants, consumables and refurbishment, repair and upgrade (RRU) cargo Global Aerospace Corporation 6 KTN - NIAC Annual Meeting - June 5, 2001
  • 6. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation CONCEPT MOTIVATION • Create permanent elements of a Mars transportation system • Take advantage of natural orbital physics to facilitate Mars transportation • Eliminate need for new, expensive class of rockets and launchers • Offer environmentally safe technology, without political baggage, for transportation to and from mars • Increase reliance on in situ resources for Mars transportation architecture • Accelerate the timeframe for permanent inhabitation of Mars Global Aerospace Corporation 7 KTN - NIAC Annual Meeting - June 5, 2001
  • 7. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation KEYS TO THE CURRENT CONCEPT • Cycler orbits between Earth and Mars that enable fast, frequent transfers between these planets • Astronaut hotels, or Astrotels, which are small transport vehicles capable of carrying 10 people on cycling orbits between planets • Orbital spaceports at the planets and very small, fast, hyperbolic transfer vehicles, or taxis, between spaceports and astrotels. • Propellant and life support in situ resource manufacturing plants • Cargo vehicles that utilize low-energy, long-flighttime orbits to transport propellant and low value cargo to and from planets • Shuttles to and from spaceports and planetary surfaces Global Aerospace Corporation 8 KTN - NIAC Annual Meeting - June 5, 2001
  • 9. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation ALDRIN CYCLERS Global Aerospace Corporation 10 KTN - NIAC Annual Meeting - June 5, 2001
  • 10. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation EXAMPLE ALDRIN UP-CYCLER SEQUENCE E3 E1 M2 M4 Global Aerospace Corporation 11 KTN - NIAC Annual Meeting - June 5, 2001
  • 11. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation UP-CYCLER LOW THRUST TRAJECTORY SHAPING Thrusting Phase Coast Phase • 2nd Correction of Up Orbit • Thrust Period 430 days • Coast Period 350 days • Uncrewed During Thrusting Global Aerospace Corporation 12 KTN - NIAC Annual Meeting - June 5, 2001
  • 13. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation TRANSPORTATION ARCHITECTURE Global Aerospace Corporation 14 KTN - NIAC Annual Meeting - June 5, 2001
  • 14. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation DOWN-CYCLER PLANETARY GEOMETRY Phobos Mars Mars Spaceport Taxi Aldrin Down Cycler Mission Profile Astrotel Aldrin Down Cycler Trajectory Propulsive Delta-Vs L1 Earth Spaceport Taxi Moon Aerocapture Maneuver Earth Global Aerospace Corporation 15 KTN - NIAC Annual Meeting - June 5, 2001
  • 15. ASTROTEL CONCEPT Xenon Propellant Tank Ion Engines (Eight, 50 cm, 17 kW, 5000s) Hab Module Cargo Pod Solar Array (160 kW) Astrotel Mass: 69.1 mt Eva
  • 16. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation ION PROPULSION SYSTEM (IPS) Global Aerospace Corporation 17 KTN - NIAC Annual Meeting - June 5, 2001
  • 17. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation EXAMPLE AERO-ASSIST PROFILE AT MARS Entry Interface 125 km Begin Aero-Cruise Pitch Over to Lmax Pitch Back to L=0 Scale Exaggerated Mars 40-50 km Altitude Entry L=0 In Orbit Global Aerospace Corporation 18 KTN - NIAC Annual Meeting - June 5, 2001
  • 18. ISS TRANSHAB CONCEPT (Courtesy NASA/JSC) Modifications • Expansion of crew from 6 to 10 • 6-times volume/crew as STS • Expansion of radiation protection • Added docking port • Include Astrotel command and control systems
  • 19. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation TAXI CONCEPT: Crew Module LEAVING EARTH SPACEPORT Aeroshell (Elliptical Raked Cone) Propellant Tanks Rocket Engines (Extended Nozzle) Taxi Dry Mass: 19.1 mt Global Aerospace Corporation 20 KTN - NIAC Annual Meeting - June 5, 2001
  • 20. TAXI CREW MODULE Crew Space Equal to Apollo Docking Port Variable g-Vector Seats (10) SEAT ROTATION
  • 22. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation IN SITU RESOURCE UTILIZATION STRATEGIES • Moon --> Polar Ice – Excavate regolith, heat and extract water (10.2 kg/hr) – Electrolyze some water into O2/H2 and liquefy to LOX/LH for lunar water tanker – Liquefy and transport most water to earth spaceport • Earth Spaceport --> ~100% Sun – Electrolyze Lunar water Into O2/H2 and liquefy to LOX/LH (1.6 kg/hr) – LOX/LH storage for Taxi • Phobos --> O2-Bearing Regolith – Carbon reduction of regolith to produce O2 (23.2 kg/hr) – Liquefy to LOX and transport to Mars spaceport for storage • Mars Spaceport --> ~100% Sun – LOX/LH storage for Taxi • Mars Surface --> Water-Bearing Regolith – Excavate regolith (dunes), heat and extract water (8.1 kg/hr) – Electrolyze water into O2/H2 and liquefy to LOX/LH for Mars shuttle Global Aerospace Corporation 23 KTN - NIAC Annual Meeting - June 5, 2001
  • 24. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation MAMA Astrotels - Type 1 - Type 2 - Type n SYSTEM INTEGRATOR INPUTS OUTPUTS* ELEMENT INTERFACES Orbital Nodes - Type 1 - Type 2 - Type n Surface Facilities - Type 1 - Type 2 - Type n Ground Facilities (Earth) - Type 1 - Type 2 - Type n ISRU Systems - Type 1 - Type 2 - Type n Launch Systems - Type 1 - Type 2 - Type n Transfer & Excursion Vehicles - Type 1 - Type 2 - Type n Launch Vehicles Trajectory Analyses Propulsion Systems Power Systems Life Support Systems Other Systems * System Integrator Output includes a standard WBS-format for all architecture candidates ELEMENTS SUPPORT ANALYSES Global Aerospace Corporation 25 KTN - NIAC Annual Meeting - June 5, 2001
  • 26. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation CARGO USE PROFILE SUMMARY Location-------------> At LEO At Earth Spaceport At Mars Spaceport At Surface of Mars At Surface of Moon At Astrotels (2 vehicles) Total Cargo Requirements LOX 122,631 1,036,348 282,339 LH 17,519 148,050 40,334 Water 157,669 363,007 Xenon 245,106 5,751 Refurb Mass 149,863 37,800 80,259 54,061 5 6 7 14,692 Augmentation Tanks 107,827 107,827 Crew Consumables 1 1 9 , 1 4 0 1 1 9 , 1 4 0 Communications Satellites Total Mass Required 621,935 335,619 1,372,483 739,741 5 6 7 139,583 • Cargo requirements over 15-years • All masses in kg Global Aerospace Corporation 27 KTN - NIAC Annual Meeting - June 5, 2001
  • 27. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation CARGO DELIVERY SYSTEMS REQUIREMENTS SUMMARY Location-------------> At LEO At Earth Spaceport Delivery Systems SEP Freighter Delivered Cargo 37,800 336,135 139,583 Cargo Freighter Each Trip 5,400 48,019 19,940 Lunar Water Tanker Total 157,669 5 6 7 Lunar Water Tanker Each Trip 22,524 81 Phobos LOX Tanker Total 1,036,348 Phobos LOX Tanker Each Trip 34,545 Mars Shuttle 54,061 Mars Shuttle Each Trip 7,723 All masses in kg At Mars Spaceport At Surface of Mars At Surface of Moon At Astrotels (2 vehicles) Global Aerospace Corporation 28 KTN - NIAC Annual Meeting - June 5, 2001
  • 28. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation NIAC / NCOS COMPARISON Item NCOS Study NIAC Study Factor Cyclic Transport Vehicle Size, mt 460 70 7 Total 15-year Propellant and Consumables, mt 34,335 2,011 17 Lunar LOX Production Rate, kg/day 4,014 73 55 Phobos LOX Production Rate, kg/day 1066 189 6 Primary Power Generation Mode Nuclear Solar -- Global Aerospace Corporation 29 KTN - NIAC Annual Meeting - June 5, 2001
  • 29. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation KEY COST ASSUMPTIONS • FY 2000 dollars • Full cost accounting on all life cycle elements • Major cost elements include: – Advanced Technology Development – Flight System Development – Launch (specific launch vehicle cost of $2000/kg) – Operations (15 years, includes RRU & propellants/consumables) Global Aerospace Corporation 30 KTN - NIAC Annual Meeting - June 5, 2001
  • 30. Global Aerospace Corporation SYSTEM INTEGRATOR OUTPUT: Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation 31 KTN - NIAC Annual Meeting - June 5, 2001 8,000 RECURRING COSTS 0 1,000 2,000 3,000 4,000 5,000 6,000 7,000 Astrotel Escape Pod Earth Spaceport Mars Spaceport Taxi Mars Cargo Freighter Astrotel Cargo Freighter LEO Shuttle Lunar Water Tanker Mars Shuttle Phobos LOX Tanker Mars Base Lunar Base Lunar Water Mine L1 Electr & Storage Phobos LOX Plant Mars Surf Water Plant Mars Spaceport Storage $M
  • 31. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation SYSTEM INTEGRATOR OUTPUT: LIFE CYCLE (15 YEARS) COSTS 30,000 25,000 20,000 15,000 10,000 5,000 0 AdvTech DEVELOPMENT & LAUNCH OPERATIONS Adv Tech Dev Adv Tech Testing Flight System Design Flight Subsys Fab System Assy, Integ, Test LV Ground Facility Proc Launch & Checkout Orbital Assy, I&T Startup Ops SS Ops Refurbishment Hardware Disposal $M 4.0 Operations 3.0 Launch Services 2.0 Flight System Dev 1.0 Advanced Technology Dev Global Aerospace Corporation 32 KTN - NIAC Annual Meeting - June 5, 2001
  • 32. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation SUMMARY OF COST ESTIMATES Development ~$50B* Operations ~$40B† Total Lifecycle ~$90B¥ ____________________ * - ~$5B/yr for 10 years † - ~$3B/yr for 15 years ¥ - For reference, the “90-day Study” (1989) costs for human exploration to the Moon and Mars was estimated at ~$400B and the NASA Mars Reference Mission (1997) was estimated at ~$40B. Global Aerospace Corporation 33 KTN - NIAC Annual Meeting - June 5, 2001
  • 34. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation SIGNIFICANCE TO NASA • Facilitates human exploration to Mars and beyond • Assists the expansion of scientific knowledge by providing ready access to Mars by scientists • Provides safe, frequent and affordable access to Mars • Creates a significant element of the transportation architecture thus contributing to the establishment of a permanent human presence on Mars Global Aerospace Corporation 35 KTN - NIAC Annual Meeting - June 5, 2001
  • 35. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation PHASE II • Key Team Members – GAC – SAIC - MAMA development & costing, orbit analysis – Purdue (Dr. Longuski) - Orbit analysis – Colorado School of Mines (Dr. King) - ISRU Concepts – Dr. Michael Duke - ISRU • Key Technical Tasks – Cyclic orbit concepts and research – Advanced aero-assist concepts – ISRU system concepts development – Develop and assess transportation options – MAMA development and costing Global Aerospace Corporation 36 KTN - NIAC Annual Meeting - June 5, 2001
  • 37. Cyclical Visits To Mars via Astronaut Hotels Global Aerospace Corporation SUMMARY • This transportation architecture, along with Astrotels, enable low-cost, frequent access to Mars for scientists and explorers • System concepts have been developed that could be utilized in expedition phases of Mars exploration • This architecture provides a framework and context for future technology advance and robotic exploration • The tools developed during this study can be used to analyze and compare future technology and system options Global Aerospace Corporation 38 KTN - NIAC Annual Meeting - June 5, 2001