Main Propulsion: Difference between revisions

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====== Main Rocket Engine ======
The main propulsion engines of a [[:Category:Ships|spacecraft]] usually operate in two modes:
Main rocket engine of the ship is the core method of propulsion of a [[spaceship]]. Main engines usually operate in two modes:
 
* Interlunar mode, providing high [[propellant economy]] for hour-to-days long [[codex:burn]]s during [[glossary:interlunar]] travel, serving both as propulsion and [[artificial gravity]].
* Interlunar mode, providing high [[propellant economy]] for the extended burns during interlunar travel, serving both as propulsion and [[artificial gravity]].
* RCS support mode, providing high [[thrust]] to complement [[RCS thruster]]s of a spaceship.
*RCS support mode, sacrificing efficiency to provide high thrust for in-ring operations.
{| class="wikitable"
{{#invoke:Equipment|list|Main Propulsion
|+Main Propulsion Chart
|Name|Manufacturer|Price|Thrust|Mass|Exhaust Velocity|Propellant Consumption|Power Consumption|Thermal Consumption|Response Time|Operation Mode|Other
!Name
}}
!Price
The Z-Axial Pinch Fusion Torch (ZAP Drive) works differently than the other engines. When firing, it requires 150 MJ of power to ignite but is self-sufficient once fusion has started. Extended [[Ultracapacitor Array|capacitor arrays]] are recommended to prevent overdraw. Fusion fuel lasts for 30 minutes of thrust and can only be viewed using the [[Heads-Up Display#Elon Interstellar Model E|EIME HUD]].
!Thrust(kN)
!Exhaust Velocity(km/s)
!Propellant Consumption(kg/s)
!Power Consumption(MW)
!Thermal Consumption(GW)
!Mass
!Response Time(s)
!Flavor
|-
|ND-PNTR
|7000
|1500
|8
|187.5
|180
|6
|450
|2.1
|Pulsed thrust, Vectored thrust angle(90d)
|-
|RA-TNTRL-K37
|1500
|750
|15
|50
|100
|5.6
|1250
|0
|Pulsed thrust, integrated 4GW generator.
|-
|ND-NTTR
|30k
|3500
|7
|500
|20
|12.2
|650
|0
|Variable thrust
|-
|RA-TNTRL-K44
|40k
|1500
|18
|83.3
|100
|13.5
|1650
|0
|Pulsed thrust, Gimbal(9d)
|-
|BWM-T535
|120k
|535
|29
|18.4
|40
|8.2
|2000
|0.9
|Variable thrust, swift expensive repairs
|-
|ERS-DFMHD-2205
|175k
|2200
|14
|157.1
|120
|15.4
|2450
|0.6
|Variable thrust
|-
|MA-NMPD42
|300k
|320
|115
|2.8
|150
|18.4
|1850
|0
|Variable thrust
|-
|Experimental NPMP
|700k
|1100
|45
|24.4
|200
|24.7
|2750
|0
|Pulsed thrust
|-
|Z-Axial Pinch Fusion Torch
|1m
|800
|1250
|0.6
|x
|x
|3000
|0
|Variable thrust, gimble(30d), ignition power(150MJ), Burn time(30m)
|}
[[Category:Equipment]]
[[Category:Equipment]]

Latest revision as of 20:16, 15 November 2024

The main propulsion engines of a spacecraft usually operate in two modes:

  • Interlunar mode, providing high propellant economy for the extended burns during interlunar travel, serving both as propulsion and artificial gravity.
  • RCS support mode, sacrificing efficiency to provide high thrust for in-ring operations.
Name Manufacturer Price Thrust Mass Exhaust Velocity Propellant Consumption Power Consumption Thermal Consumption Response Time Operation Mode Other
ND-PNTR engine Nakamura Dynamics 7,000 E$ 1,500 kN 450 kg 8 km/s 187.5 kg/s 180 MW 6 GW 2.1 s Pulsed thrust Vectored thrust (90°)
RA-TNTRL-K37 engine Rusatom-Antonoff 15,000 E$ 750 kN 1,250 kg 15 km/s 50 kg/s 100 MW 5.6 GW Pulsed thrust
ND-NTTR thruster Nakamura Dynamics 30,000 E$ 3,500 kN 650 kg 7 km/s 500 kg/s 20 MW 12.2 GW Variable thrust
RA-MHFTR-K44 engine Rusatom-Antonoff 40,000 E$ 1,500 kN 1,650 kg 18 km/s 83.3 kg/s 100 MW 13.5 GW Pulsed thrust Gimbaled (9°)
BWM-T535 BWM 120,000 E$ 535 kN 2,000 kg 29 km/s 18.4 kg/s 0.04 MW 8.2 GW 0.9 s Variable thrust Integrated turbine
ERS-DFMHD-2205 Electro Ride Systems 175,000 E$ 2,200 kN 2,450 kg 14 km/s 157.1 kg/s 120 MW 15.4 GW 0.6 s Variable thrust
MA-NMPD42 engine Mitsudaya-Starbus 300,000 E$ 320 kN 1,850 kg 115 km/s 2.8 kg/s 150 MW 18.4 GW Variable thrust
Experimental NPMP engine Elon Interstellar 700,000 E$ 1,100 kN 2,750 kg 45 km/s 24.4 kg/s 200 MW 24.7 GW Pulsed thrust
Z-Axial Pinch fusion torch Elon Interstellar 1,000,000 E$ 800 kN 3,000 kg 1,250 km/s 0.6 kg/s Variable thrust Gimbaled (30°), fusion drive with 30min burn time

The Z-Axial Pinch Fusion Torch (ZAP Drive) works differently than the other engines. When firing, it requires 150 MJ of power to ignite but is self-sufficient once fusion has started. Extended capacitor arrays are recommended to prevent overdraw. Fusion fuel lasts for 30 minutes of thrust and can only be viewed using the EIME HUD.

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