Editing Talk:1461: Payloads

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:::Ok, I'm just about following you I think! So assuming we are launching to orbit, we have to get to 23,600km, at which point gravity is considerably reduced. We definately have to take into account {{w|Space elevator#Apparent gravitational field|change in gravity}} as our horses move up the cable.
 
:::Ok, I'm just about following you I think! So assuming we are launching to orbit, we have to get to 23,600km, at which point gravity is considerably reduced. We definately have to take into account {{w|Space elevator#Apparent gravitational field|change in gravity}} as our horses move up the cable.
  
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:::I did some maths, and I believe it takes 19.9GJ to get a 450kg horse to 23,600km. That is essentially mgh, but taking into account the change in gravity. At 1 Watt, thats gonna take 631 years. Our 500 horses per year solar plant needs to output 315kW ([http://www.solardaily.com/reports/Independence_Solar_Completes_300_kW_Rooftop_Solar_Array_999.html 300kW solar array on a roof for reference]). Our 10 horses per minute power station would need to output 3.32GW, so a decent nuclear facility. Once the Three Gorges Dam in China is running at full capacity (22.5GW), it could be launching 68 horses per minute. Running constantly at full capacity, we could rid the world of horses (est 58 million) in under two years. --[[User:Pudder|Pudder]] ([[User talk:Pudder|talk]]) 11:09, 19 December 2014 (UTC)
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:::I did some maths, and I believe it takes 19.9GJ to get a 450kg horse to 23,600km. That is mgh, but taking into account the change in gravity. At 1 Watt, thats gonna take 631 years. Our 500 horses per year solar plant needs to output 315kW (High, but possible). Our 10 horses per minute power station would need to output 3.32GW, so a decent nuclear facility. Once the Three Gorges Dam in China is running at full capacity (22.5GW), it could be launching 68 horses per minute. Running constantly at full capacity, we could rid the world of horses (est 58 million) in under two years. --[[User:Pudder|Pudder]] ([[User talk:Pudder|talk]]) 11:09, 19 December 2014 (UTC)
  
 
:::I confirmed the height of 23 600 km with my own calculations; my result is about 189 km altitude at perigeum, and 996 km for 24 350 km (750 km higher, as you wrote). My code seems consistent as entering geostationary orbit altitude results in geostationary orbit. Anyway, I think that 19.9 GJ is slightly wrong - [http://www.wolframalpha.com/input/?i=G*earth+mass*450+kg+*+(1%2Fearth+radius-1%2F(earth+radius%2B23600km)) I entered it into Wolfram], and it showet a little more. This results in 350 kW and 3.7 GW for backyard solar panels and power plant, respectively. [[Special:Contributions/162.158.92.100|162.158.92.100]] 22:20, 28 January 2017 (UTC)
 
:::I confirmed the height of 23 600 km with my own calculations; my result is about 189 km altitude at perigeum, and 996 km for 24 350 km (750 km higher, as you wrote). My code seems consistent as entering geostationary orbit altitude results in geostationary orbit. Anyway, I think that 19.9 GJ is slightly wrong - [http://www.wolframalpha.com/input/?i=G*earth+mass*450+kg+*+(1%2Fearth+radius-1%2F(earth+radius%2B23600km)) I entered it into Wolfram], and it showet a little more. This results in 350 kW and 3.7 GW for backyard solar panels and power plant, respectively. [[Special:Contributions/162.158.92.100|162.158.92.100]] 22:20, 28 January 2017 (UTC)

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