S
SpaceTas
Guest
The flexible path mission envisioned is to a near earth object, with a few days travel time there and back.
These objects are small; less than a km across. So the surface gravity is very low. For a 1 km object with the density of Phobos (1.9 g.cm^3) the escape velocity is only 0.515 m/s (1.8 km/h 1.15 mi/hr) ie a fast walking pace. This is the speed needed to jump 0.0135m on Earth (lifting body's center of mass 1.3 cm == a little bit over an inch). This is easy. So the astronauts will have trouble moving about: maybe a shuffle rather than a moonwalk ! Manned Maneuvering Units, tethers and anchors will be needed. All this gear has already been used on Mir, Soyuz, Shuttle or ISS.
So an asteroid mission is like docking to a tumbling dirty station with no ready built hand rails. The advantage is no lander needed; "just" some grappling system. There will be some "fancy flying" needed to match the rotation of the asteroid especially if it very irregular in shape; eg if you land in a saddle you'll feel the gravity force from below and the sides of the saddle. Doable; ie NEAR and Hayabusa.
The energy/time needed to reach asteroid and return depends a lot on the asteroid's orbit and the capabilities of the spacecraft. The best would be an asteroid with an orbit closely matching (similar inclination and period) that of the Earth.
The current designs are skewed toward a lunar mission; which only requires 2 weeks (max) duration and the fuel for the Moon and back. So this would severely limit your options.
Here's a question for MeteorWayne: How many NEO's are know with inclinations < 10 deg and periods within 10% of 1 year.?
These objects are small; less than a km across. So the surface gravity is very low. For a 1 km object with the density of Phobos (1.9 g.cm^3) the escape velocity is only 0.515 m/s (1.8 km/h 1.15 mi/hr) ie a fast walking pace. This is the speed needed to jump 0.0135m on Earth (lifting body's center of mass 1.3 cm == a little bit over an inch). This is easy. So the astronauts will have trouble moving about: maybe a shuffle rather than a moonwalk ! Manned Maneuvering Units, tethers and anchors will be needed. All this gear has already been used on Mir, Soyuz, Shuttle or ISS.
So an asteroid mission is like docking to a tumbling dirty station with no ready built hand rails. The advantage is no lander needed; "just" some grappling system. There will be some "fancy flying" needed to match the rotation of the asteroid especially if it very irregular in shape; eg if you land in a saddle you'll feel the gravity force from below and the sides of the saddle. Doable; ie NEAR and Hayabusa.
The energy/time needed to reach asteroid and return depends a lot on the asteroid's orbit and the capabilities of the spacecraft. The best would be an asteroid with an orbit closely matching (similar inclination and period) that of the Earth.
The current designs are skewed toward a lunar mission; which only requires 2 weeks (max) duration and the fuel for the Moon and back. So this would severely limit your options.
Here's a question for MeteorWayne: How many NEO's are know with inclinations < 10 deg and periods within 10% of 1 year.?