Discussion Overview
The discussion explores the feasibility of observing Earth as it orbits the Sun from a spacecraft, specifically considering the location and speed required for such an observation. Participants raise questions about the mechanics of maintaining a specific velocity relative to Earth and the visual effects of Earth's rotation during this observation.
Discussion Character
- Exploratory
- Technical explanation
- Conceptual clarification
- Debate/contested
Main Points Raised
- Abhay questions the possibility of watching Earth approach at 50 km/h and asks about the necessary location and speed of the spacecraft.
- One participant suggests that the spacecraft's speed should be 50 km/h towards Earth, but warns that being too close would result in falling towards it, while being too far would lead to a different orbit around the Sun.
- Another participant calculates that starting 1.4 million km away would allow Earth to appear the same size as the Moon, but notes that maintaining a speed of 50 km/h would require thrust to counteract gravitational influences from both Earth and the Sun.
- There is a discussion about the complexity of Earth's orbit, including the need for multi-directional thrusts to maintain position relative to Earth, and the implications of placing the spacecraft at L1 for fuel efficiency.
- Some participants mention that the spacecraft would need to account for various velocities, including the Sun's motion and the motion of the Milky Way galaxy, although one argues that these larger motions are not significant for the spacecraft's immediate concerns.
Areas of Agreement / Disagreement
Participants generally agree on the complexity of the scenario and the need for thrust to maintain a specific velocity towards Earth. However, there is no consensus on the most fuel-efficient approach or the exact mechanics involved, indicating multiple competing views and unresolved questions.
Contextual Notes
The discussion involves assumptions about gravitational influences, the spacecraft's trajectory, and the nature of orbits, which are not fully resolved. The calculations and proposed methods are contingent on various factors that remain unspecified.