Jump to content

Sweetie bot

Members
  • Posts

    44
  • Joined

  • Last visited

Posts posted by Sweetie bot

  1. On 6/3/2020 at 2:26 PM, OOM said:

    As an example, I take a space power station with a nuclear reactor (and also something like a load like an ion engine or a microwave transmitter) - with good cooling, your radiators will stop accumulating temperature at ~ 1100K

    I more likely to put that temperature higher, and just use enough radiators Area to make a good Power/Mass Ratio.

  2. On 5/13/2020 at 7:36 PM, FreeThinker said:

    exactly where did you get this number from?

    according to this document, iso will not be higher than 211s

     

    that numbuer just some theoretically Max,like that LOX/ LH 2 Rocket Combustion in chemical equilibrium can get 510s + at max 100% Eff

    Sorry I dont make that clear:blush:

    v2-bfcdfb71a71eb81e38946a0fbee343fc_720w

    pic from :https://zhuanlan.zhihu.com/p/67562119

    I just look again, it a Solid CO Mix LOX, thing might get different

     

  3. 5 minutes ago, FreeThinker said:

    Alright, I think I fixed it

    c0d1CdO.jpg

    As you can see it now only produces 2.16 MW, equal to the maximum electric power of the generator which is configured at 1% (weighting only 0.179 t).

     

    Wow that a really Quickly  Fix, how can u do that   :P

    So quick that For Now we just made some free time to watch Space X Lunch there New Firewor..... Eh... The New test rocket that will gona Booooom (in plan)soon.:cool:

  4. Long time not see :P

    First I want to say that New UI of Propellant selection are really great to use, I really appreciate it :wink:

    And that TEG come with Variable installed capacity also very useful for build light weight craft. But still look like has some minor bug like, when u reduce that capacity of generator to 20%, that reactor still been require as 100% power, and that rest of Heat Power beem turn in to Waste heat , that make those generator are not beem reduce  capacity but efficiency as -80%,

     

    For example:Heat to MJ power efficiency with 20% capacity of TEG:

    A Reactor that with Max 100MW  HeatPower, TEG current  efficiency in 50%,capacity 20%

    ideal:   H×20% , 0.2H × 50%      Reactor run in 20MW to support 20% capacitygen to get 10MW power. Waste heat 10MW

    current: H ×(50%×20%)                   Reactor run in 100MW to support 20% capacity gen to get 10MW power. Waste heat 90MW.

    "H"as  Reactor power level.

    Result in a lot of waste for energy and Over Heat Radiator......

  5. On 11/1/2019 at 6:51 AM, FreeThinker said:

    KSPIE 1.24.1 is now avaialable for Kerbal Space Program 1.8.1

    Released on 2019-10-31

    • Compiled against KSP 1.8.1
    • Balance: Reduced mass and cost Magneto Inertial Fusion Engine
    • Balance: Reduced drag and mass Thermal Receiver dish
    • Balance: Reduced fuel storage and fuel efficiency Pebblebed reactor
    • Fixed several gray (DDS) textures
    • Fixed texture, time warp animation, and power warning on Magneto Inertial Fusion Engine
    • Fixed Fusion Engines Filter extension

    LOL I  remember that Deinonychus 1-D Chem Eng was put in Fusion Engines type, some how feel that partly correct because they have operate in a similar way —— by putting two thing together to make it heat up and eject out.

  6. On ‎1‎/‎13‎/‎2019 at 1:49 AM, blowfish said:

    Ah right, for those engines Squad hid the old ones and the new ones are entirely new parts.  So they need configs.

    Temporary solutions, If you have Filter Extensions and switch to Squad tag for all part you can see that old part . that can be show that old part still here and have RF feature.

    Perhaps that is another bug by Filter Extensions  that cause Failure to hide old part :/.(but helpful)

  7. On ‎1‎/‎7‎/‎2019 at 12:44 AM, Friznit said:

    I just ran into this problem as well (KSP 1.5.1) .  In some cases the RFBR (aka Timberwind) reactor stops generating Thermal Power - Reactor Status in the Reactor Control Window shows Active (0.00%), whereas a normal working Timberwind usually shows (0.020%) when idle, producing a steady 12KW of TP.  If you shut the reactor down, the decay heating kicks in and starts generating thermal power for a few days until it cools off.  Unfortunately I can't reliably reproduce the issue after various tests of reloading, warping, switching vessels etc .  If I can figure out a way to do so and catch it in the logs I'll update the post.

    Same Problems, when you open debug— you will see " [KSPI]-managed ProvidedPowerSupplyPer SecondMiniMumRatio illegal Values." that flash very fast and push over other messages.

    Is that kind of Bug?

    Edit:

    I running on KSP 1.4.5, Have RSS and RF,That ship have  pebblebed  in 1.25m, MIF Fusion Engine 2.5m,2 CANDLE as payload use(Tiny airless lander). one TEFR 0.625m on payload. Pebblebed and TEFR Have no power and lock in Active (0.00%). No fuel consume on Power Generator . However that MIF still can use and work normal.

    other Solid core NTR are normal too.

  8. On 6/24/2018 at 2:16 AM, FreeThinker said:

    Version 1.19.3 for Kerbal Space Program 1.4.3 can be downloaded from here

    Released on 2018-06-23

    • Compiled against KSP 1.4.4
    • Included new PhotonSail plugin, which reintroduces the SolarSail with improved realism and ability to be propelled by Bea med power
    • Added Replaced hard coded Field Strength modifiers by configurable modifiers
    • Fixed Magnetic Field Strength initialization (credits by Jumberjack)

    Hello, I was playing ksp 1.3.1. And I can't find SolarSail or PhotonSail in Vab and R&D,is that not included in 1.3.1 yet?

  9. On 2018/3/12 at 6:50 PM, Sweetie bot said:

     

    Second idear is about Chemical combustion reactor. You can think it as a close cycle rocket engine or reactor but power by chemical. When run it produce TP by combining chemical fuel and re-collection Combustion product(Like Water, CO2, etc) . Can link to TEG for cover to MJ, or link to Thermal nozzle. Core Temp Decide on combustion type, can have a cap on 3200K (Not on MHD)

    If this Link to Thermal nozzle that can be a new evolution of chemical engines:cool:You get the engine power by Chemical combustion but Isp and propellant same as Soild NTR! 

     

    Ex:

    Let burn H2 to get heat

    H2+O2=H2O(recovery) + Heat(3200+K)

    Recover water then heat propellant directly through heat exchanger ;

    propellant+Heat(3200+K) = thrust with high Exhaust velocity

    get thrust and isp same or even higher than NTR, and not lossing much propellant

    ideal to handel some low △DV orbital transfer

     

     

    If you like you can even burn a coal (Carbon) to power your Steam Rocket !!:P

    By burn some soild fuel and heat propellant directly through heat exchanger.

    C + O2= CO2↑ + Heat 

    it also recover that carbon to some product that is easy to handle.

     

     

    After some long time thinking , I re-think about what I'm going to say.

     

    The way to improve that  Chemical rocket efficiency (in weight way) is reduce oxidizer.

     

    To do that, first we need make sure  that  "fuel" are way more than "oxidizer", and then we don't use oxidizer as a propellant, because it high in molar mass will reduce ISP for engine. I think that a jump out the box to thinking.

    How to do that? By reuse that oxidizer again. burn fuel and oxdizer in a close system and them let Heat heat up propellant (normally fuel) by pass heat exchanger. Result high Exhaust velocity and low mass follow. Get lot thermal Power to use, and  byproduct like water Steam and CO2 need storage, and electrolyze that to get back oxidizer in idle time.

     

    Overall:

    ①A engine that Isp and TWR similar as solid core NTR but it a chemical! It mean no need of rad shied and Eco-friendly, and no special resources are needed.(because nuclear fuel are rare.

    ②Reducing the risk that fission fuels are easily owned by civilians, it might be use to trade in black market and be use to make a bomb in some secret place.

    ③Burning time are limited(by how many oxidizer and byproduct storage  can use in one time ). So It might burn muti time rather than one burn to finish orbital transfer.

    ④Low in Technical, rare resoure requite.

    ⑤tradeoff to reduce Overall power to get mass saving.

    ⑥ In theory it can use any propellant ! ( rather them few combustion for chemical rocket)

  10. On 2018/3/13 at 6:22 AM, Arivald Ha'gel said:

    Once you'll do the research, you'll notice that energy density of chemical reaction is way to small for such an idea to be feasible. Even if you could transfer energy efficiently from combustion products - what you can't do efficiently, and using Termal Power Generator wouldn't be that great

    Well, I designed the main purpose of the device Not only for energy, but also recover that cryogenic fuel  back to Easy to store fuel (such as waterwith higher density and boiling point, save on tank mass and Volume. In this case energy is a by-product. It can be electrolyzed againg by some low and stable power supply.( Like charging a giant battery/ Regenerative Fuel Cells)

    And also, even that fuel combustion energy density are low, but the power ratio for combustion should way more higher then early reactor.  In futher, we can have MPD generator to deal with some high adiabatic flame temperature such as H2+F2 (8000+K).

     As alway. In space Energy are cheep, but Materials are expensive.

  11. Hello there, After some long time thinking and explosion , I have got some new ideas for Energy harvesting from Chemical Power.

    First is about Oversize Fuel cell. That's very obvious,It can conversion  H2+O2 to water, Power and wasteheat. And it can also use Hydrazine as fuel too.Ex:Hydrazine Fuel cells

     

    Second idear is about Chemical combustion reactor. You can think it as a close cycle rocket engine or reactor but power by chemical. When run it produce TP by combining chemical fuel and re-collection Combustion product(Like Water, CO2, etc) . Can link to TEG for cover to MJ, or link to Thermal nozzle. Core Temp Decide on combustion type, can have a cap on 3200K (Not on MHD)

    If this Link to Thermal nozzle that can be a new evolution of chemical engines:cool:You get the engine power by Chemical combustion but Isp and propellant same as Soild NTR! 

     

    Ex:

    Let burn H2 to get heat

    H2+O2=H2O(recovery) + Heat(3200+K)

    Recover water then heat propellant directly through heat exchanger ;

    propellant+Heat(3200+K) = thrust with high Exhaust velocity

    get thrust and isp same or even higher than NTR, and not lossing much propellant

    ideal to handel some low △DV orbital transfer

     

     

    If you like you can even burn a coal (Carbon) to power your Steam Rocket !!:P

    By burn some soild fuel and heat propellant directly through heat exchanger.

    C + O2= CO2↑ + Heat 

    it also recover that carbon to some product that is easy to handle.

     

     

    More thing i will add after research

    Purpose:

    Fit the gap between Solar power, Low power reactor and Capacitance,New way to Handle Chemical fuel (like burn secend stage Hydron fuel to easy storage water), Give more Fun on low tech experience.

     

    Tech tree:

    Both Unlock at High power ec system same with TEG,  can be update by tech

  12. On 2017/9/20 at 11:34 AM, FreeThinker said:

    I'm using a bit less optimistic version

    Spot size = distance-to-spot * wavelength / (aperture diameter)

    I wonder where the 0.61 comes from

    Perhaps a more accurate formula would be

    1.22 * distance-to-spot * wavelength / (aperture diameter)

    :PAlright, Got that, I try to make a Excel witch wavelength Eff Range to help choice ideal beam type.

  13. On 2017/10/10 at 10:06 PM, juanml82 said:

    I've tried that, but it's still not working. I've used hyperedit to erase all the waste heat, just in case, but it makes no difference. I don't have a KSPI fission reactor on board as well, but if that was needed, why was I able to depart Kerbin and capture at Neidon? What does the error means?

    MYLGctT.png

    Maybe you can try to use a small fission reactor (Motle salt or else) to power the Fusion reactor, than power main engine?

  14. I am doing localization tutorial  and for now it part for Beam power, I try to make a equations form on excel , Is this Equations I choose correct? 

    RT = 0.61 * D * L / RL

    where:

    RT = beam radius at target (m)

    D = distance from laser emitter to target (m)

    L = wavelength of laser beam (m, see table below)

    RL = radius of laser lens or reflector (m)

    http://www.projectrho.com/public_html/rocket/spacegunconvent.php#id--Laser_Cannon--Equations

×
×
  • Create New...