#physics

physics are interesting sciences

• Model: Artistic

• Size: 896 X 704 (0.63 MP)

• Used settings:

  • Prompt: physics are interesting sciences
  • Face enhance: No
  • Upscale & Enhance: 0
  • Aspect Ratio: landscape

Implosion

• Model: Stable

• Size: 960 X 640 (0.61 MP)

• Used settings:

  • Prompt: light two nucleus virus particles tethered by energy pulse plasma, artistic, dominant blue color style, cosmos
  • Face enhance: No
  • Upscale & Enhance: 0
  • Aspect Ratio: landscape

Wormhole from a far-away planetary system

• Model: PhotoReal

• Size: 1248 X 832 (1.04 MP)

• Used settings:

  • Prompt: Realistic wormhole without accreation disk, spacecraft approaching from distance, space empty with only one bright star and a few dim stars
  • Using base image: Yes (Effect strength - 50%)
  • Base image resolution: Default
  • Face enhance: Yes
  • Upscale & Enhance: 0
  • Aspect Ratio: landscape

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

• Used settings:

  • Prompt: With lift-off mass of 210,000 kg (460,000 lb), Ariane 1 was able to put in geostationary transfer orbit one satellite or two smaller of a maximal weight of 1,850 kg (4,080 lb). The cost of program is estimated at 2 billion euros. The Ariane 1 was a four-stage vehicle (fourth stage put satellite from GTO to GEO is usually not counted as part of rocket, because it is included in 1,850 kg of payload). The first stage was equipped with 4 Viking engines developed by the Société Européenne de Propulsion. The second stage had a single Viking engine. The third stage had one LOX/LH2 bipropellant engine capable of a thrust of 7,000 kgf (69 kN; 15,000 lbf). This design was kept in the Ariane series until Ariane 4.
  • Using base image: Yes (Effect strength - 40%)
  • Base image resolution: Default
  • Face enhance: No
  • Upscale & Enhance: 0
  • Aspect Ratio: landscape

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

• Used settings:

  • Prompt: A space station is a spacecraft capable of supporting a human crew in orbit for an extended period of time, and is therefore a type of space habitat. It lacks major propulsion or landing systems. An orbital station or an orbital space station is an artificial satellite (i.e. a type of orbital spaceflight). Stations must have docking ports to allow other spacecraft to dock to transfer crew and supplies. The purpose of maintaining an orbital outpost varies depending on the program. Space stations have most often been launched for scientific purposes, but military launches have also occurred.
  • Using base image: Yes (Effect strength - 40%)
  • Base image resolution: Default
  • Face enhance: No
  • Upscale & Enhance: 0
  • Aspect Ratio: landscape

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

• Used settings:

  • Prompt: Heat Transportation - The Pump Module (PM) provides flow and accumulator functions and maintains proper temperature control at the pump outlet for each Loop. The PM consists of a single pump, a fixed charge accumulator, a Pump & Control Valve Package (PCVP) containing a firmware controller, startup heaters, isolation valves, and various sensors for monitoring performance. The Nitrogen Tank Assembly (NTA) controls the flow of ammonia out of the Ammonia Tank Assembly (ATA). The ATA contains two flexible, chambers incorporated into its ammonia tanks that expand as pressurized nitrogen from the NTA expels liquid ammonia out of the ATA. The major components in the ATA include two ammonia storage tanks, isolation valves, heaters, and various temperature, pressure, and quantity sensors.
  • Using base image: Yes (Effect strength - 40%)
  • Base image resolution: Default
  • Face enhance: No
  • Upscale & Enhance: 0
  • Aspect Ratio: landscape

Ukraine, Kotsiubiiv, Kotsiubiiv O & B Theatre

• Model: Artistic

• Size: 1024 X 576 (0.59 MP)

• Used settings:

  • Prompt: The International Space Station (ISS) External Active Thermal Control System (EATCS)[1] maintains an equilibrium when the ISS environment or heat loads exceed the capabilities of the Passive Thermal Control System (PTCS). Note Elements of the PTCS are external surface materials, insulation such as Multi-Layer Insulation (MLI), or Heat Pipes. The EATCS provides heat rejection capabilities for all the U.S. pressurized modules, the Japanese Experiment Module (JEM), the Columbus Orbital Facility (COF), and the main power distribution electronics of the S0, S1 and P1 Trusses.
  • Using base image: Yes (Effect strength - 40%)
  • Base image resolution: Default
  • Face enhance: No
  • Upscale & Enhance: 0
  • Aspect Ratio: landscape

Cosmic Vortex

• Model: DreamForge

• Size: 896 X 704 (0.63 MP)

• Used settings:

  • Prompt: blackhole
  • Face enhance: No
  • Upscale & Enhance: 0
  • Aspect Ratio: landscape