Sub-orbital Spaceflight - Orbit

Orbit

During freefall the trajectory is part of an elliptic orbit as given by the orbit equation. The perigee distance is less than the radius of the Earth R including atmosphere, hence the ellipse intersects the Earth, and hence the spacecraft will fail to complete an orbit. The major axis is vertical, the semi-major axis a is more than R/2. The specific orbital energy is given by:

where is the standard gravitational parameter.

Almost always a < R, corresponding to a lower than the minimum for a full orbit, which is

Thus the net extra specific energy needed compared to just raising the spacecraft into space is between 0 and .

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