Launch Vehicle Technical Data - CobaltWolf/Bluedog-Design-Bureau GitHub Wiki
Payload capacity (kg)
Tested at full throttle (thrust reduced in VAB where appropriate), no restarts on non-restartable engines, fairings held to > 60,000 meters. Fuel reduced where necessary when TWR limits payload. Payload placed into 100km circular orbit. Ascent Performed with Mechjeb Ascent Guidance.
Name | Real LEO | LKO | LKO 3.0x |
---|---|---|---|
Scout | 210 | 214 | 110 |
Vanguard/Viklun | 9 | 278 *1 | 100 *2 |
Juno/Chryslus II | 41 | 648 | 50 |
Thor/Fenris Able/Alpha |
120 | 1,500 | x |
Thor/Fenris Ablestar/Alphastar |
150 | 2,000 | x |
Thor/Fenris Agena/Belle A |
250 | 1,700 | 250 |
Thor/Fenris Agena/Belle B |
400 | 2,000 | 644 |
Thor/Fenris Agena/Belle D |
1,150 | 1,750 | 740 |
Thrust-Augmented Thor/Fenris (3x Castor) Agena/Belle D |
1,500 | 2,750 | 918 |
Thorad/Fenris (LT Thor, 3x Castor) Agena/Belle D |
3,000 | 3,250 | 1,256 |
Athena/Minerva 1 | 820 | 1,580 | 776 |
Athena/Minerva 2 | 2,065 | 2,550 | 1,580 |
Delta/Daleth II 7320 | 2,800 | 4,730 | 2,100 |
Delta/Daleth II 7920 | 4,850 | 6,830 | 2,600 |
Titan/Prometheus II | 3,100 | 5,450 | 3,128 |
- 2 stage Vanguard/Able
- 3 stage Vanguard/Able/Alcyone