Draft:Saturn INT-05
| Function | Launch vehicle for Apollo |
|---|---|
| Country of origin | United States |
| Size | |
| Height | 190 feet (58 m) (w/o payload) |
| Diameter | 21.68 feet (6.61 m) |
| Mass | 4,009,700 pounds (1,818,800 kg) gross (to LEO) |
| Capacity | |
| Payload to LEO | |
| Mass | 94,873 pounds (43,034 kg) |
| Associated rockets | |
| Family | Saturn |
| Launch history | |
| Status | Study, not developed |
| Launch sites | Kennedy Space Center |
| First stage – AJ-260X | |
| Height | 99.99 feet (30.48 m) |
| Diameter | 21.6 feet (6.6 m) |
| Empty mass | 334,198 pounds (151,590 kg) |
| Gross mass | 3,634,000 pounds (1,648,000 kg) |
| Powered by | 1 AJ-260X |
| Maximum thrust | 7,956,302.132 pounds-force (35,391.39512 kN) |
| Specific impulse | 289 secs |
| Burn time | 114 seconds |
| Propellant | Solid |
| Second stage – S-IVB | |
| Height | 58.3 feet (17.8 m) |
| Diameter | 21.68 feet (6.61 m) |
| Empty mass | 28,400 pounds (12,900 kg) |
| Gross mass | 261,900 pounds (118,800 kg) |
| Powered by | 1 J-2 |
| Maximum thrust | 231,913 pounds-force (1,031.60 kN) |
| Burn time | 475 seconds |
| Propellant | LH2 / LOX |
The Saturn INT-05 was a concept rocket studied by NASA. It took the form of a Saturn IB with the S-IB stage replaced by a 260 inch (6.6 meter) solid rocket motor.
See also
[edit]References
[edit]- Bibliography
Encyclopedia Astronautica Saturn INT-05
| Early proposals |  | |
|---|---|---|
| "C" series | ||
| Saturn I series | ||
| Saturn II series | ||
| Saturn V series | ||