Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Saturn INT-19
Part of Saturn V
Saturn 2SL Minuteman
Saturn 2SL Minuteman
Saturn 2SL Minuteman strapons
Credit: © Mark Wade
North American study, 1966. Saturn variant with 4 to 12 Minuteman motors as boosters, Saturn II stage as core, and Saturn IVB upper stage. Saturn II stage would be fitted with lower expansion ratio engines and would ignite at sea level. Various combinations of numbers of strap-ons, propellant loading of the two core stages were studied.

Status: Study 1966. Payload: 34,320 kg (75,660 lb). Thrust: 9,061.41 kN (2,037,086 lbf). Gross mass: 770,000 kg (1,690,000 lb). Height: 51.00 m (167.00 ft). Diameter: 10.06 m (33.00 ft). Apogee: 185 km (114 mi).

Liftoff Mass - kgMM Motors at LiftoffMM Motors 2nd RoundMM Motors 3rd RoundS-II Propellant - kgS-IVB Propellant - kgPayload - kg
328,300---188,20077,1005,500
463,50022-217,70080,30013,200
579,60042-277,60076,60020,100
579,60044-236,70073,00018,100
722,90062-367,80076,60027,200
722,90064-318,40078,00026,800
734,200642294,80081,20023,100
722,90066-273,90078,90025,400
866,70084-410,90080,70028,800
866,70084-410,90075,70033,700
866,70084-410,90075,20034,200

LEO Payload: 34,320 kg (75,660 lb) to a 185 km orbit at 28.00 degrees.

Stage Data - Saturn INT-19



Family: orbital launch vehicle. People: von Braun. Country: USA. Engines: J-2-SL. Stages: Saturn II-SL, Saturn IVB (S-IB), M55/TX-55/Tu-122.
Photo Gallery

Saturn 2 w MM SOSaturn 2 w MM SO
Credit: © Mark Wade



Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use