asteroid tour trajectory d. hyland nov 21, 2012. voyage concepts we sketch potential trajectories...
TRANSCRIPT
![Page 1: Asteroid Tour Trajectory D. Hyland Nov 21, 2012. Voyage Concepts We sketch potential trajectories for our deep space vessel: –Initial voyage from LEO](https://reader035.vdocuments.net/reader035/viewer/2022072006/56649d0d5503460f949e227d/html5/thumbnails/1.jpg)
Asteroid Tour Trajectory
D. Hyland
Nov 21, 2012
![Page 2: Asteroid Tour Trajectory D. Hyland Nov 21, 2012. Voyage Concepts We sketch potential trajectories for our deep space vessel: –Initial voyage from LEO](https://reader035.vdocuments.net/reader035/viewer/2022072006/56649d0d5503460f949e227d/html5/thumbnails/2.jpg)
Voyage Concepts
• We sketch potential trajectories for our deep space vessel:– Initial voyage from LEO to Sun-Earth L2– Repetitive grand tour of Near Earth Asteroids (mining
operations)
• Calculations are based on the patched Planar Circular Restricted Three Body Problem (PCR3BP) method.
• Additional guidance from:– Past missions (e.g. Genesis)– Published mission concepts (Earth-Moon L1 to Sun-Earth L2,
Jupiter orbiter – see Koon, Lo, Marsden and Ross)– Astronomical observations (e.g. Jupiter comet Oterma)
![Page 3: Asteroid Tour Trajectory D. Hyland Nov 21, 2012. Voyage Concepts We sketch potential trajectories for our deep space vessel: –Initial voyage from LEO](https://reader035.vdocuments.net/reader035/viewer/2022072006/56649d0d5503460f949e227d/html5/thumbnails/3.jpg)
Planar Circular Restricted Three Body Problem (PCR3BP)
![Page 4: Asteroid Tour Trajectory D. Hyland Nov 21, 2012. Voyage Concepts We sketch potential trajectories for our deep space vessel: –Initial voyage from LEO](https://reader035.vdocuments.net/reader035/viewer/2022072006/56649d0d5503460f949e227d/html5/thumbnails/4.jpg)
The Jacobi Integral: Five Cases of Possible Motions
![Page 5: Asteroid Tour Trajectory D. Hyland Nov 21, 2012. Voyage Concepts We sketch potential trajectories for our deep space vessel: –Initial voyage from LEO](https://reader035.vdocuments.net/reader035/viewer/2022072006/56649d0d5503460f949e227d/html5/thumbnails/5.jpg)
Initial Deployment: Spiral out to E-M L1
3385 10 km
Start in 300 km circular orbit about Earth
Spiral out to a coasting trajectory to the E-M L1 “throat”.
Meld into the Lyapunov orbit of L1 Station and refuel
![Page 6: Asteroid Tour Trajectory D. Hyland Nov 21, 2012. Voyage Concepts We sketch potential trajectories for our deep space vessel: –Initial voyage from LEO](https://reader035.vdocuments.net/reader035/viewer/2022072006/56649d0d5503460f949e227d/html5/thumbnails/6.jpg)
From E-M L1 to S-E L2: Start of the First grand Tour
Moon
L1 Lyapunov Orbit
Orbit of the Moon
Earth-Moon Frame Sun-Earth Frame
L2
L2
L1
Sun
E-L1 to S-L2: V=12m/s, 50 days
122,720 km
After refueling, leave L1 on the outward invariant manifold.
Swing by the Moon and exit the E-M L2 throat in time to meld with a heteroclinic orbit leading to the Sun-Earth L2
Take one turn around the Lyapunov orbit and enter the external domain of the Sun-Earth system
![Page 7: Asteroid Tour Trajectory D. Hyland Nov 21, 2012. Voyage Concepts We sketch potential trajectories for our deep space vessel: –Initial voyage from LEO](https://reader035.vdocuments.net/reader035/viewer/2022072006/56649d0d5503460f949e227d/html5/thumbnails/7.jpg)
Sun-Earth System
Asteroid Mining Tours: Exterior Realm
L1
1. Drop off cargo at L1 Station. Leave L1 Lyapunov orbit. Follow heteroclinic orbit to L2 (pink line, left to right) (drop off cargo at Earth-Moon system)
2. Meld into L2 Lyapunov orbit, follow for ¾ of a period, then follow the unstabile manifold (green line, heading down)
Sun-Earth Frame
L2
3.0 million km
![Page 8: Asteroid Tour Trajectory D. Hyland Nov 21, 2012. Voyage Concepts We sketch potential trajectories for our deep space vessel: –Initial voyage from LEO](https://reader035.vdocuments.net/reader035/viewer/2022072006/56649d0d5503460f949e227d/html5/thumbnails/8.jpg)
Through S-E L2 to the Grand Tour of the Exterior Realm
Sun
3-2 resonance
Apophis
3. Follow the homoclinic, exterior domain orbit (green path issuing from L2 and going clockwise)
4. Mine Atens and Apollos on the way (3 years)
Then: see next slide
1 AU
![Page 9: Asteroid Tour Trajectory D. Hyland Nov 21, 2012. Voyage Concepts We sketch potential trajectories for our deep space vessel: –Initial voyage from LEO](https://reader035.vdocuments.net/reader035/viewer/2022072006/56649d0d5503460f949e227d/html5/thumbnails/9.jpg)
Sun-Earth System
Heteroclinic Transfer Between Exterior and Interior Realms
L1
5. Follow homoclinic exterior domain orbit to L2 on the stable manifold (green line, pointing down, left). Refurbish and repair at L2 Station
6. Meld into L2 Lyapunov orbit, follow for ½ of a period, then follow the heteroclinic orbit to L1 (pink line, right to left).
7. Deliver cargo to Earth-Moon system. Meld into L1 Lyapunov orbit, Exchange crew and refuel at L1 Station.
8. Follow Lyapunov orbit for one period, then follow the homoclinic interior domain orbit (blue line heading to the left)
L2
3.0 million km
![Page 10: Asteroid Tour Trajectory D. Hyland Nov 21, 2012. Voyage Concepts We sketch potential trajectories for our deep space vessel: –Initial voyage from LEO](https://reader035.vdocuments.net/reader035/viewer/2022072006/56649d0d5503460f949e227d/html5/thumbnails/10.jpg)
Through S-E L1 to the Grand Tour of the Interior Realm
Sun
3-2 resonance
Apophis
9. Follow the homoclinic, interior domain orbit (red path issuing from L1 and going counter clockwise)
10. Mine Atens and Amors on the way (two years)
11. Then follow the stable manifold to L1 (blue line in previous slide, heading to the right).
12. Refuel and exchange crew at L1 station.
Go to step 1 and repeat.
Forbidden zone