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formal statement (Lean)
47noncomputable def thermal_thrust : ℝ :=
proof body
Definition body.
48 spacecraft_thermal_power * thermal_asymmetry / c_speed
49
50/-- Resulting acceleration (m/s²). a = F / m for ~1000 kg spacecraft -/
used by (5)
From the project-wide theorem graph. These declarations reference this one in their body.
depends on (7)
Lean names referenced from this declaration's body.
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c_speed
in IndisputableMonolith.Experimental.FlybyAnomaly
decl_use
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spacecraft_thermal_power
in IndisputableMonolith.Experimental.FlybyAnomaly
decl_use
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thermal_asymmetry
in IndisputableMonolith.Experimental.FlybyAnomaly
decl_use
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for
in IndisputableMonolith.Foundation.UniversalForcingSelfReference
decl_use
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F
in IndisputableMonolith.Physics.AnchorPolicy
decl_use
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F
in IndisputableMonolith.Physics.LeptonGenerations.TauStepDerivation
decl_use
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F
in IndisputableMonolith.Pipelines
decl_use