Regulus I RGM-6 SSM-N-8
| Specifications | ||
|---|---|---|
|
|
English |
Metric |
|
Dimensions |
||
|
Wingspan (ft/m) |
21 |
6.40 |
|
Overall Langth (ft/m) |
34.4 |
10.49 |
|
Height (ft/m) |
8.3 |
2.53 |
|
Fuselage Diameter (ft/m) |
4.71 max |
1.44 |
|
Weights and Capacities |
||
|
Empty Weight (lb/kg) |
6618 |
3002 |
|
Launching Gross Weight (lb/kg) |
13812 |
6265 |
|
Flight Gross Weight (lb/kg) |
11671 |
5294 |
|
Fuel Capacity (gal/l) |
310 |
1173 |
|
Powerplant Characteristics |
||
|
Type: Allison J33-A-14 or -18A |
||
|
Rating : Thrust at sea level (lb/newton) |
4600 |
20462 |
|
Weight (lb/kg) |
|
|
|
Size (length~in X diameter~in) |
|
|
|
Performance |
||
|
Maximum Speed at35,000 ft (knot) |
543 |
|
|
Time to climb to 35,000 ft (min) |
11.5 |
|
|
Max Range at 35,000 ft, Mach .85 (nautmi) |
520 |
|
|
Max Mach during terminal dive from 35,000 ft |
1.15 |
|
|
|
|
|
|
Crew: |
||
|
Armament: |
||
|
Model |
1950 |
1952 |
1953 |
1954 |
1955 |
1956 |
1957 |
Total |
|
XSSM-N-8 |
5 |
10 |
15 |
4 |
1 |
|
|
35 |
|
XSSM-N-8a |
|
|
1 |
9 |
|
|
|
10 |
|
SSM-N-8 |
|
|
|
19 |
59 |
36 |
60 |
174 |
|
SSM-N-8a |
|
|
|
11 |
93 |
62 |
52 |
218 |
|
KDU-1 |
|
|
|
|
41 |
32 |
4 |
77 |
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Total |
5 |
10 |
16 |
43 |
194 |
130 |
116 |
514 |
|
NOTES: |
||||||||
|
XSSM-N-8 - Experimental Flight Test Missile |
||||||||
|
NEWSLETTER
|
| Join the GlobalSecurity.org mailing list |
|
|
|

