HELIOSmatics 2

24F(d,p)25F@10MeV/u

Beam (A):		Beam Ex:		MeV
Target (a):
Light (b):		Q-value:	2.057	MeV
Heavy (B):	25F

HELIOS

SOLARIS

ISS

B-field (abs.):		T
Beam Energy:		MeV/u

E_x [MeV]	θ_cm[deg]	E_b[MeV]	Z_b0[mm]	Z_b[mm]	2ρ_b[mm]	θLab_b[deg]	T_b[ns]	E_B[MeV]	θLab_B[deg]	Z_B0/2[mm]	2ρ_B[mm]

θ_CM:		deg
Array Pos:		mm
Recoil Pos:		mm

Recoil radius, inner [mm]:

outter [mm]:

zRange can be changed by Array position.

eRange:

MeV

zRange(Min):		mm
zRange(Max):		mm
rRange:		mm

DWBA and Monte Carlo Simulation

DWBA and E_x List:

Positive parity Negative parity Unknown parity
Max Ex: MeV

Beam J^π:

E_x [MeV]	J^π	Orbital

Incoming Channel
Outgoing Channel

Cal. DWBA ONLY Cal. DWBA

min θ_CM		[deg]
max θ_CM		[deg]

Plot config:

E vs Z	Ex (cal.)	ThetaCM
ThetaCM vs Z	Recoil X vs Y	Recoil-R vs ThetaCM
Recoil R vs Z	Time diff vs Z	Array X vs Y

Array Hit
Loop = 1
ThetaCM > 10 deg

θ_CM Calculator

The calculation only give θ_CM after the bending.

Ex [MeV] :

θ_CM Gate [deg] :

X Gate [%] :

pos₀(gated)

pos₁(gated)

θ₁[deg]

θ₂[deg]

θ_avg[deg]

Δθ[deg]

sin(θ_avg)Δθ

HELIOSmatics was first built by Ben P. Kay in MS Excel around 2010. It was modified by Ryan Tang later. And now it migrated to the web on Dec, 2022.
The calculation can be found in the source code (heliosmatics.js or press F12)