diff --git a/functions/miscellaneous/createDissileInput.m b/functions/miscellaneous/createDissileInput.m index 69fa5ca36503b83d940b1e788242352289598e15..39bc2b0b88f53030d739d657bdb7668c3fae7f6f 100644 --- a/functions/miscellaneous/createDissileInput.m +++ b/functions/miscellaneous/createDissileInput.m @@ -167,6 +167,6 @@ input.fltcon.NMACH = length(input.fltcon.MACH); %% OPTIONS input.printTxt = false; % if you want the coefficients printed in the command window input.draw = false; % if you want the shape of your rocket plotted -input.HREflag = rocket.motor.isHRE; +input.HREflag = rocket.motor.type == MotorType.Hybrid; input.axibod.precision = 11; % [-] 1-1001, how many points to approximate nose cone shape, default is 11 (NOTE: POWER SHAPE REQUIRES <= 401) end diff --git a/missions/2025_Orion_Portugal_October/data/aeroCoefficients.mat b/missions/2025_Orion_Portugal_October/data/aeroCoefficients.mat index 38e3cadeaccf86b460758fd3cd82a75c2c2568c2..b3c1b232046a3a87cdee3944653945372648719d 100644 --- a/missions/2025_Orion_Portugal_October/data/aeroCoefficients.mat +++ b/missions/2025_Orion_Portugal_October/data/aeroCoefficients.mat @@ -1,3 +1,3 @@ version https://git-lfs.github.com/spec/v1 -oid sha256:2334c819e3d9d1979e4b405971fd7d8ebbf16f29e8b6ac7fd88042a71adb925a -size 288256257 +oid sha256:75ad0a581c512de8f345a79f16d8e3d2bf681547eb386ce000434c66d6b292e0 +size 288267248 diff --git a/missions/2025_Orion_Portugal_October/data/aeroCoefficientsHighAOA.mat b/missions/2025_Orion_Portugal_October/data/aeroCoefficientsHighAOA.mat index 0e19b88f5f5f46202b068c433b45056d0853ee15..9bd98f086dcafb9f9cdb22dcf40d83a9c8ea127d 100644 --- a/missions/2025_Orion_Portugal_October/data/aeroCoefficientsHighAOA.mat +++ b/missions/2025_Orion_Portugal_October/data/aeroCoefficientsHighAOA.mat @@ -1,3 +1,3 @@ version https://git-lfs.github.com/spec/v1 -oid sha256:39c4c9f66b48648cd44891a9b6357eac741428283a2829d1eab4fdb655c520e0 -size 40434681 +oid sha256:da4a2977b055341314ba88e9698ffbac9702c2e57e9b876c67ea2da01631b783 +size 40438794