Make Talon engines BEEFIER

code/modules/overmap/ships/engines/gas_thruster_vr.dm

@@ -0,0 +1,71 @@
+//These connect at the corner 2 steps and 3 steps in the dir from their loc
+/obj/machinery/atmospherics/unary/engine/bigger
+	name = "large rocket nozzle"
+	desc = "Advanced rocket nozzle, expelling gas at hypersonic velocities to propel the ship."
+	icon = 'icons/turf/shuttle_parts64.dmi'
+	icon_state = "engine_off"
+	
+	volume_per_burn = 30
+	charge_per_burn = 6000
+	boot_time = 70
+
+	bound_width = 64
+	bound_height = 64
+
+/obj/machinery/atmospherics/unary/engine/bigger/atmos_init()
+	if(node)
+		return
+
+	var/node_connect = dir
+	var/turf/one_step = get_step(src,node_connect)
+
+	for(var/obj/machinery/atmospherics/target in get_step(one_step,node_connect))
+		if(can_be_node(target, 1))
+			node = target
+			break
+
+	update_icon()
+	update_underlays()
+
+/obj/machinery/atmospherics/unary/engine/bigger/burn()
+	. = ..()
+	if(.)
+		icon_state = "engine_on"
+		spawn(2 SECONDS)
+			icon_state = initial(icon_state)
+
+/obj/machinery/atmospherics/unary/engine/biggest
+	name = "huge rocket nozzle"
+	desc = "Enormous rocket nozzle, expelling gas at hypersonic velocities to propel the ship."
+	icon = 'icons/turf/shuttle_parts96.dmi'
+	icon_state = "engine_off"
+	
+	volume_per_burn = 50
+	charge_per_burn = 10000
+	boot_time = 100
+
+	bound_width = 96
+	bound_height = 96
+
+/obj/machinery/atmospherics/unary/engine/biggest/burn()
+	. = ..()
+	if(.)
+		icon_state = "engine_on"
+		spawn(2 SECONDS)
+			icon_state = initial(icon_state)
+
+/obj/machinery/atmospherics/unary/engine/biggest/atmos_init()
+	if(node)
+		return
+
+	var/node_connect = dir
+	var/turf/one_step = get_step(src,node_connect)
+	var/turf/two_step = get_step(one_step,node_connect)
+
+	for(var/obj/machinery/atmospherics/target in get_step(two_step,node_connect))
+		if(can_be_node(target, 1))
+			node = target
+			break
+
+	update_icon()
+	update_underlays()

code/modules/overmap/ships/engines/thermal.dm

@@ -1,99 +0,0 @@
-//Thermal nozzle engine
-/datum/ship_engine/thermal
-	name = "thermal engine"
-
-/datum/ship_engine/thermal/get_status()
-	..()
-	var/obj/machinery/atmospherics/unary/engine/E = engine
-	return "Fuel pressure: [E.air_contents.return_pressure()]"
-
-/datum/ship_engine/thermal/get_thrust()
-	..()
-	var/obj/machinery/atmospherics/unary/engine/E = engine
-	if(!is_on())
-		return 0
-	var/pressurized_coef = E.air_contents.return_pressure()/E.effective_pressure
-	return round(E.thrust_limit * E.nominal_thrust * pressurized_coef)
-
-/datum/ship_engine/thermal/burn()
-	..()
-	var/obj/machinery/atmospherics/unary/engine/E = engine
-	return E.burn()
-
-/datum/ship_engine/thermal/set_thrust_limit(var/new_limit)
-	..()
-	var/obj/machinery/atmospherics/unary/engine/E = engine
-	E.thrust_limit = new_limit
-
-/datum/ship_engine/thermal/get_thrust_limit()
-	..()
-	var/obj/machinery/atmospherics/unary/engine/E = engine
-	return E.thrust_limit
-
-/datum/ship_engine/thermal/is_on()
-	..()
-	var/obj/machinery/atmospherics/unary/engine/E = engine
-	return E.on
-
-/datum/ship_engine/thermal/toggle()
-	..()
-	var/obj/machinery/atmospherics/unary/engine/E = engine
-	E.on = !E.on
-
-//Actual thermal nozzle engine object
-
-/obj/machinery/atmospherics/unary/engine
-	name = "engine nozzle"
-	desc = "Simple thermal nozzle, uses heated gast to propell the ship."
-	icon = 'icons/obj/ship_engine.dmi'
-	icon_state = "nozzle"
-	var/on = 1
-	var/thrust_limit = 1	//Value between 1 and 0 to limit the resulting thrust
-	var/nominal_thrust = 3000
-	var/effective_pressure = 3000
-	var/datum/ship_engine/thermal/controller
-
-/obj/machinery/atmospherics/unary/engine/Initialize()
-	. = ..()
-	controller = new(src)
-
-/obj/machinery/atmospherics/unary/engine/Destroy()
-	..()
-	controller.die()
-
-/obj/machinery/atmospherics/unary/engine/proc/burn()
-	if (!on)
-		return
-	if(air_contents.temperature > 0)
-		var/transfer_moles = 100  * air_contents.volume/max(air_contents.temperature * R_IDEAL_GAS_EQUATION, 0,01)
-		transfer_moles = round(thrust_limit * transfer_moles, 0.01)
-		if(transfer_moles > air_contents.total_moles)
-			on = !on
-			return 0
-
-		var/datum/gas_mixture/removed = air_contents.remove(transfer_moles)
-
-		loc.assume_air(removed)
-		if(air_contents.temperature > PHORON_MINIMUM_BURN_TEMPERATURE)
-			var/exhaust_dir = reverse_direction(dir)
-			var/turf/T = get_step(src,exhaust_dir)
-			if(T)
-				new/obj/effect/engine_exhaust(T,exhaust_dir,air_contents.temperature)
-		return 1
-
-//Exhaust effect
-/obj/effect/engine_exhaust
-	name = "engine exhaust"
-	icon = 'icons/effects/effects.dmi'
-	icon_state = "exhaust"
-	anchored = 1
-
-	New(var/turf/nloc, var/ndir, var/temp)
-		set_dir(ndir)
-		..(nloc)
-
-		if(nloc)
-			nloc.hotspot_expose(temp,125)
-
-		spawn(20)
-			loc = null