# HELIOSmatics

# 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 |

Ex [MeV] | θcm[deg] | Eb[MeV] | Zb0[mm] | Zb[mm] | 2ρb[mm] | θLabb[deg] | Tb[ns] | EB[MeV] | θLabB[deg] | ZB0/2[mm] | 2ρB[mm]
--- | --- | --- | --- | --- | --- | --- | --- | --- | --- | --- | ---

θCM: |  | 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 |

# θCM Calculator

The calculation only give θCM after the bending.

Ex [MeV] : |  | θCM Gate [deg] : |  | X Gate [%] : |

ID | pos0(gated) | pos1(gated) | θ1[deg] | θ2[deg] | θavg[deg] | Δθ[deg] | sin(θavg)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)