shut up skystar
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你先把還在審核中(Pending) or Help map的RANK才能繼續上傳新的MAPhvick225 wrote:
我花了很久的時間
製作了一首歌
但是上傳缺發生問題
跑出一個視窗 上面寫
An error occurred:
Yoy have exceeded your submission cap(you are currently allowed 2 total unranked maps). Please finish the maps you have currently submitted, or ask a mod(onirc or in the thread) to have them graveyarded if you no longer wish to complete them
我把它翻譯成中文有點怪怪的
想問一下是怎麼回事
為甚麼不能上船?
↖上傳數目到上限就不能在上傳了
若沒有rank map情況下，pending or Help map存有二個你的map就無法繼續上傳
RANK MAP 1個 上傳上限2→3
RANK MAP 2個 上傳上限3→4
RANK MAP 3個 上傳上限4→5
最高數為5
而在graveyard則不計
abalee補充:成為subscription還可以多三個上傳map的位子
話說我更新還會有人爬到嗎..(小聲
Topic Starter
This map has been deleted on the request of its creator. It is no longer available.
This map has been deleted on the request of its creator. It is no longer available.
維可愛
維可愛
shut up skystar
shut up skystar
ill hit skystar's quan
The Tsiolkovsky rocket equation, classical rocket equation, or ideal rocket equation, describes the motion of vehicles that follow the basic principle of a rocket: a device that can apply acceleration to itself using thrust by expelling part of its mass with high velocity and thereby move due to the conservation of momentum.
The equation relates the delta-v (the maximum change of velocity of the rocket if no other external forces act) with the effective exhaust velocity and the initial and final mass of a rocket, or other reaction engine.
For any such maneuver (or journey involving a sequence of such maneuvers):
where:
(The equation can also be written using the specific impulse instead of the effective exhaust velocity by applying the formula
where 
is the specific impulse expressed as a time period and g 0 {\displaystyle g_{0}} g_{0} is standard gravity = 9.80665 m/s2.)
The equation relates the delta-v (the maximum change of velocity of the rocket if no other external forces act) with the effective exhaust velocity and the initial and final mass of a rocket, or other reaction engine.
For any such maneuver (or journey involving a sequence of such maneuvers):
where:
is delta-v – the maximum change of velocity of the vehicle (with no external forces acting).
is the initial total mass, including propellant, also known as wet mass.
is the final total mass without propellant, also known as dry mass.
is the effective exhaust velocity.
is the natural logarithm function.
(The equation can also be written using the specific impulse instead of the effective exhaust velocity by applying the formula