diff --git a/julia/src/inner_loop/inner_loop.jl b/julia/src/inner_loop/inner_loop.jl
index eca8409..c0ba6f5 100644
--- a/julia/src/inner_loop/inner_loop.jl
+++ b/julia/src/inner_loop/inner_loop.jl
@@ -44,7 +44,7 @@ function inner_loop(launch_date::DateTime,
   end
 
   time = utc2et(Dates.format(launch_date,"yyyy-mm-ddTHH:MM:SS"))
-  thrust_profiles = []
+  thrust_profiles = Vector{Matrix{Float64}}()
 
   for phase in phases
     planet1_state = [spkssb(ids[phase.from_planet], time, "ECLIPJ2000"); 0.0]
diff --git a/julia/test/inner_loop/inner_loop.jl b/julia/test/inner_loop/inner_loop.jl
index c612697..26c503d 100644
--- a/julia/test/inner_loop/inner_loop.jl
+++ b/julia/test/inner_loop/inner_loop.jl
@@ -47,15 +47,14 @@
 
   # The first leg should be valid
   fresh_sc = copy(sc)
-  mass, thrusts = inner_loop( launch_date,
-                              sc,
-                              start_mass,
-                              [phase1],
-                              verbose=true,
-                              mbh_specs=(25,50) )
-  @test sc.mass > sc.dry_mass
-  path, final = prop(thrusts[1], earth_state+[zeros(3);v∞s[1]], fresh_sc, μs["Sun"], leg1_tof)
-  @test final ≈ p1_state + [zeros(3); v∞s[2]]
+  thrusts = inner_loop( launch_date,
+                        sc,
+                        start_mass,
+                        [phase1],
+                        verbose=true,
+                        mbh_specs=(25,50) )
+  path, final = prop(thrusts[1], earth_state+[zeros(3);v∞s[1];0.0], Sc("test"), μs["Sun"], leg1_tof)
+  @test final[1:6] ≈ p1_state[1:6] + [zeros(3); v∞s[2]]
   savefig(plot_orbits(  [earth, p1_path, path],
                 primary="Sun",
                 labels=["Earth", p1, "Leg 1"],