G – H – I– J – K – L – M – other
G Motor Thrust to Weight Ratios
| Motor Type | Mfg. | Max. Weight LBS
(5:1) |
Max. Weight GRAMS (5:1) | Initial Thrust (lbs.) | Average Thrust (lbs.) |
| G25 (n) | Aerotech | 1.08 | 490 | 12 | 5.4 |
| G33 (r) (n) | Aerotech | 1.36 | 617 | 12 | 6.8 |
| G35 (n) | Aerotech | 1.52 | 689 | 17 | 7.6 |
| G40 (n) | Aerotech | 1.46 | 662 | 14 | 7.3 |
| G40 | Kosden | 1.66 | 753 | 13 | 8.3 |
| G54 (r) (n) | Aerotech | 2.16 | 980 | 15 | 10.8 |
| G55 (n) | Aerotech | 2.1 | 953 | 16 | 10.5 |
| G60 (r) | Cesaroni | 2.92 | 1,325 | 16 | 14.6 |
| G64 (r) (n) | Aerotech | 2.86 | 1,297 | 14.3 | |
| G65 (r) | Kosden | 3.14 | 1,424 | 15.7 | |
| G70 (n) | NCR | 3.14 | 1,424 | 19 | 15.7 |
| G75 (r) | Aerotech | 2.98 | 1,352 | 17 | 14.9 |
| G75 (r) | Kosden | 3.36 | 1,524 | 20 | 16.8 |
| G80 (n) | Aerotech | 3.68 | 1,669 | 24 | 18.4 |
* Estimated Performance; inadequate data available
(r) indicates reloadable motor
(n) indicates NAR
Shaded areas indicate motors are no longer certified by TMT and will not be allowed for launches after 8/31/01.
