This mission sees the Pheonix launch an 85 ton payload to between 100 and 120km orbit. A single 3 degree gravity turn at 30m/s is enough to achieve orbit, with booster separation at 30km, and after payload deploy the core stage will land in the general vacinity of the launchpad with a parachute assisted final descent.
The entire mission is automated, including camera angle, throttle down for maxQ, booster seperation, orbit insertion burn, reentry burn, slowdown burn, and landing.
GENERAL INFO
- Predecessor: Phoenix SuperHeavy
- Successors 4 craft(s)
- Created On: Android
- Game Version: 0.8.402.0
- Price: $73,327k
- Number of Parts: 127
- Dimensions: 86 m x 15 m x 15 m
PERFORMANCE
- Total Delta V: 15.2km/s
- Total Thrust: 25.9MN
- Engines: 22
- Wet Mass: 1.36E+6kg
- Dry Mass: -210,996kg
STAGES
Stage | Engines | Delta V | Thrust | Burn | Mass |
---|---|---|---|---|---|
1 | 15 | 13.2km/s | 23.6MN | 4.5m | 1.36E+6kg |
2 | 0 | 0m/s | 0N | 0s | 9.09E+5kg |
3 | 1 | 2.0km/s | 1.5MN | 3.8m | 2.36E+5kg |
9 Comments
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17 Lkninml
So that was a new experience. Nicely done. Any thoughts on a fully automated Apollo mission? I have never had a single sucsessful docking so my command pod, lunar dock and land dream has not been possible.
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8,458 crowxe
@batwolf
Any time :) . Look at my video "the Luna job automated" just skip to finalising the orbit or the more sensitive moment of extending the apogee to 36,000 km without over shooting. -
270 batwolf
@crowxe Awesome, thank you, I'll try that on my new project I'm working on :)
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8,458 crowxe
neat program. here's a trick for approaching required values like perigee to equal apogee . set throttle to {2% + (apogee-perigee)/apogee} when the 2 values almost equal it will be (x-x)/x or added thrust equal zero besides the 2% you put yourself , this prevents overshooting required values due to game lag or engines specs
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@Lkninml thanks, that is my goal but I'm still learning how to do all the parts of the mission. Vizi does not five us location data so i don't know how to automate docking... Yet