What is the InterPlanetary Superhighway?
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1 What is the InterPlanetary Superhighway? Kathleen Howell Purdue University Lo and Ross
2 Trajectory Key Space Technology Mission-Enabling Technology Not All Technology is hardware!
3 The InterPlanetary Superhighway (IPS) Low Energy Orbits for Space Missions i InterPlanetary Superhighway a vast network of winding tunnels in space that connects the Sun, the planets, their moons, AND many other destinations Systematic mapping properly known as InterPlanetary Transport Network Simó, Gómez, Masdemont / Lo, Howell, Barden / Howell, Folta / Lo, Ross / Koon, Lo, Marsden, Ross / Marchand, Howell, Lo / Scheeres, Villac/.
4 Originates with Poincaré (1892) Applications to wide range of fields Different View of Problems in N-Bodies Much more than Kepler and Newton imagined Computationally challenging Poincaré ( ) NBP Mathematics is the art of giving the same name to different things Jules Henri Poincaré Play Wang 3BP 2BP New Era in Celestial Mechanics
5 Pioneering Work: Numerical Exploration by Hand (Breakwell, Farquhar and Dunham)
6 Current Libration Point Missions Goddard Space Flight Center z WIND SOHO ACE MAP GENESIS NGST Courtesy of D. Folta, GSFC
7 Multi-Body Problem Change our perspective Orbit propagated for 4 conic periods: 4*19 days = 75.7 days Earth Earth Sun To Sun Rotating Rotating View View (Rotates t with two bodies) Inertial View Inertial View Aeronautics and Astronautics
8 Multi-Body Problem Change our perspective Effects of added gravity fields Earth Earth To Sun Rotating View Inertial View
9 Equilibrium Points
10 Play #1
11 Zoom in here!
12
13 Sputnik Orbit
14 Periodic Orbits Exist (Locate on Poincaré Sections)
15 Periodic Orbits Exist
16 Zoom into Earth region Earth Select any particular orbit To Sun
17 Sun-Earth Halo Orbits Earth To Sun Play #2 Any 3B System Play #3 Surface Play #4
18 Sun-Earth Halo Orbits Sun Earth Infinite Number Of Orbits - Create Surface
19 Each Orbit: Each Orbit: -Additional Surface - Interesting and Very Useful -Orbit
20 To Sun
21 Select one Periodic Orbit 3D Halo Orbit Earth To Sun Key is Unstable Nature
22 Point Along Orbit Represents Fixed Point - One Stable Mode - Compute Trajectory in Negative Time - Compute for All Points - Creates Another Surface Transfer Trajectories - Asymptotic Arrival
23 Play #5
24 Note Tubular Structure
25 Stable Mode
26 Unstable Mode
27 Sun-Earth System L1 Halo orbit Family Infinite Number of Orbits Infinite Number of Orbits Select Any Orbit for Use! u
28 Trajectory Design: Select one Periodic Orbit from each L1 and L2 Families Earth 3D Halo Orbit 3D Halo Orbit To Sun Key is Unstable Nature
29 L1 Unstable
30 L2 Stable
31 Play #6
32
33 Earth Lo and Ross
34 Genesis Launch: Aug 8, 2001 Landing: Sept 8, 2004
35 Purdue University Genesis Design JPL Earth to L1 Halo L1 Lunar Orbit Halo Orbit
36 GENESIS Nominal Mission Trajectory View from N. Ecliptic (Z-axis) 1 Y To Sun 6 1, 15, halo orbit lunar orbit X parking orbit (option) Launch TCM-1 TCM-2 TCM 3 TCM-3 TCM-4 Halo Orbit Insertion (TCM-5) Begin Science Phase End Science Phase Halo Orbit Departure (TCM-6) TCM-7 TCM 8 TCM-8 TCM-9 TCM-10 TCM-11 Entry Backup Entry L+30d Transfer Return Recovery 01/07/01 01/07/01 01/14/01 01/21/01 04/13/01 04/23/01 04/30/01 03/22/03 04/01/03 04/15/03 06/10/03 07/20/03 08/09/03 08/18/03 08/19/03 09/07/03 Science 0.5 Z To Sun X View from Anti-Earth Velocity (-Y-axis) Axis, in millions of kilometers: X = Sun-Earth Line, positive anti-sun Y = (Z) x (X) Z = Ecliptic Normal View from Anti-Sun (X-axis) 1
37
38 GENESIS Nominal Mission Trajectory View from N. Ecliptic (Z-axis) 1 Y To Sun 6 1, 15, halo orbit lunar orbit X parking orbit (option) Launch TCM-1 TCM-2 TCM 3 TCM-3 TCM-4 Halo Orbit Insertion (TCM-5) Begin Science Phase End Science Phase Halo Orbit Departure (TCM-6) TCM-7 TCM 8 TCM-8 TCM-9 TCM-10 TCM-11 Entry Backup Entry L+30d Transfer Return Recovery 01/07/01 01/07/01 01/14/01 01/21/01 04/13/01 04/23/01 04/30/01 03/22/03 04/01/03 04/15/03 06/10/03 07/20/03 08/09/03 08/18/03 08/19/03 09/07/03 Science 0.5 Z To Sun X View from Anti-Earth Velocity (-Y-axis) Axis, in millions of kilometers: X = Sun-Earth Line, positive anti-sun Y = (Z) x (X) Z = Ecliptic Normal View from Anti-Sun (X-axis) 1
39
40 Purdue University Genesis Design Earth to L1 Halo JPL L1 Lunar Orbit Halo Orbit L1 Halo to Earth Landing Lunar Orbit L L Earth 2 1 Halo Orbit Portal JPL Lagrange Group
41 GENESIS Nominal Mission Trajectory View from N. Ecliptic (Z-axis) 1 Y To Sun 6 1, 15, halo orbit lunar orbit X parking orbit (option) Launch TCM-1 TCM-2 TCM 3 TCM-3 TCM-4 Halo Orbit Insertion (TCM-5) Begin Science Phase End Science Phase Halo Orbit Departure (TCM-6) TCM-7 TCM 8 TCM-8 TCM-9 TCM-10 TCM-11 Entry Backup Entry L+30d Transfer Return Recovery 01/07/01 01/07/01 01/14/01 01/21/01 04/13/01 04/23/01 04/30/01 03/22/03 04/01/03 04/15/03 06/10/03 07/20/03 08/09/03 08/18/03 08/19/03 09/07/03 Science 0.5 Z To Sun X View from Anti-Earth Velocity (-Y-axis) L1 Unstable L2 Stable Axis, in millions of kilometers: X = Sun-Earth Line, positive anti-sun Y = (Z) x (X) Z = Ecliptic Normal Then View from Anti-Sun (X-axis) L2 Unstable for Return 1
42
43 Also Natural Objects: Also Natural Objects: Sun-Jupiter System some comets follow manifold tube structure Lo Talk Thurs
44 Switch to a mission using SE L2 WMAP
45 WMAP Nominal mission: 27 months + several years extension Total Payload ~ 830 kg WMAP instruments continuously shaded from the Sun, Earth, and Moon to lower thermal disturbances To Sun
46 WMAP Sun Shield Proposed 1995 WMAP Delta II Rocket Launch Launched June 30, 2001 Kennedy Spaceflight Center Launch, Pad 17B Almost perfect launch -- on time to the sec
47 To Sun
48 WMAP Spacecraft Trajectory
49 Play #7 WMAP Trajectory
50 Move to Future? Earth-Moon Systemm EM L1 Gateway
51 Space Station at EM L1 Gateway Approach To Earth Docked at EM L1 Gateway
52 Telescope Ops at Libration Points Advanced Telescope Array at SE L2 To Sun L2
53 Advanced Telescope Stationed at SE L2 Serviced at EM L1 Gateway
54 Libration Points in Earth s Neighborhood Every 3-Body System: 5 Fixed Libration Points Generate the InterPlanetary Superhighway M. Lo
55 EM L1 Gateway Hub Connect through tubes! SE L2 Telescope Station
56 Play #8 Lo and Ross
57 Human Servicing at Lunar L 1 Gateway Build Instruments & S/C Lunar L 1 Gateway for EL 2 Service S/C at Earth L 2 from Lunar L 1 Gateway Module LUNAR L 1 GATEWAY EARTH L 2 HALO ORBIT MOON LUNAR L 1 HALO ORBIT LUNAR L 2 HALO ORBIT EARTH Lo and Ross
58 Following Tubes Lo and Ross
59 Earth-Moon L1 Gateway Hub
60 Lander at Earth-Moon L1 Gateway Station
61 Transfer Vehicle Docked at Gateway-1 Transfer Vehicle Docked at Gateway-2
62 InterPlanetary Superhighway (IPS) Planets; Moons within Planetary Systems Lo and Ross
63 Spacecraft Between Earth and Moon Ride on Surfaces in Space (Ozimek and Howell, Purdue University)
64 Manifold Surfaces in Earth-Moon System (Ozimek and Howell, Purdue University)
65 L1 Gateway Station!!! We Want You!!!
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