Difference between revisions of "Planetary Launch Procedures"
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− | ==== | + | ====Planetary Launch Procedure==== |
# Follow procedures in [[P1.5.3]] and [[P1.5.4.1]] steps 1 to 5 | # Follow procedures in [[P1.5.3]] and [[P1.5.4.1]] steps 1 to 5 | ||
# Select the current planet as reference and target object (see [[P1.5.4.1]]) | # Select the current planet as reference and target object (see [[P1.5.4.1]]) | ||
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#* If V<sub>hab-ref</sub> is more than V<sub>o ref</sub>, use reverse thrust to decrease V<sub>hab-ref</sub>. | #* If V<sub>hab-ref</sub> is more than V<sub>o ref</sub>, use reverse thrust to decrease V<sub>hab-ref</sub>. | ||
# Stop engines. | # Stop engines. | ||
+ | |||
+ | [[Category:Procedures]] |
Latest revision as of 17:00, 26 April 2013
Planetary Launch Procedure
- Follow procedures in P1.5.3 and P1.5.4.1 steps 1 to 5
- Select the current planet as reference and target object (see P1.5.4.1)
- Press F4 for automatic depart from target orientation.
- Press 'v' to activate approach velocity vector.
- Increase thrust to exceed local gravity by at least 1 m/s2 and AYSE drive will lift off.
- Adjust thrust to maintain the desired lift-off speed.
- Press F1 for manual orientation control.
- Gradually rotate the AYSE drive counter-clockwise until the orientation is perpendicular to the direction back to the planet.
- Press F2 for automatic ccw orbit ref orientation.
- If the approach velocity vector is pointing away from the planet:
- Press F3 for automatic approach to targ orientation.
- Use slight thrust to restore correct approach velocity vector.
- If the approach velocity vector is pointing towards the planet:
- Press F4 for automatic depart from ref orientation.
- Use slight thrust to restore correct approach velocity vector.
- Press F2 to restore automatic ccw orbit ref orientation.
- If Vhab-ref is less than Vo ref, use positive thrust to increase Vhab-ref.
- If Vhab-ref is more than Vo ref, use reverse thrust to decrease Vhab-ref.
- Stop engines.