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🔴 Patreon: 👕 “Rawlmart“ merch store: 🔵 PayPal: 👍 Like ✅ Subscribe 🔔 Activate Notifications Vintage raw footage of the 1969 launch of the Apollo 11 Saturn V rocket which carried astronauts Neil Armstrong, Buzz Aldrin, and Michael Collins to the Moon. Armstrong and Aldrin landed the lunar module “Eagle“ and became the first humans to set foot on another celestial body. Collins piloted the command module “Columbia“ in its orbit around the Moon. Apollo 11 video playlist: Saturn V Info ~~~~~~~~~~~ Cost per launch: $ (adjusted for 2019) Height: 110.6 m (363.0 ft) Diameter: 10.1 m (33.0 ft) Mass: 2,970,000 kg (6,540,000 lb) Payload to LEO: 140,000 kg (310,000 lb) Payload to TLI: 48,600 kg (107,100 lb) First/Last Flights: Nov 9, 1967 - May 14, 1973 13 launches, 12 successes, 1 partial failure (Apollo 6) Saturn V First Stage (S-IC) ~~~~~~~~~~~~~~~~~ Height: 42.1 m (138 ft) Diameter: 10.1 m (33 ft) Dry mass: 130,000 kg (287,000 lb) Launch mass: 2,290,000 kg (5,040,000 lb) Engines: 5 Rocketdyne F-1 Thrust (sea level): 35,100 kN (7,891,000 lbf) Specific impulse (sea level): 263 seconds ( km/s) Burn time: 168 seconds Fuel: RP-1 / LOX Manufacturer: Boeing Saturn V Second Stage (S-II) ~~~~~~~~~~~~~~~~~~~~ Height: 24.8 m (81.5 ft) Diameter: 10.1 m (33 ft) Dry mass: 40,100 kg (88,400 lb) Launch mass: 496,200 kg (1,093,900 lb) Engines: 5 Rocketdyne J-2 Thrust (vacuum): 5,141 kN (1,155,800 lbf) Specific impulse (vacuum): 421 seconds ( km/s) Burn time: 360 seconds Fuel: LH₂ / LOX Manufacturer: North American Aviation Saturn V Third Stage (S-IVB) ~~~~~~~~~~~~~~~~~~~ Height: 18.8 m (61.6 ft) Diameter: 6.6 m (21.7 ft) Dry mass: 15,200 kg (33,600 lb) Launch mass: 123,000 kg (271,000 lb) Engines: 1 Rocketdyne J-2 Thrust (vacuum): 1,033.1 kN (232,250 lbf) Specific impulse (vacuum): 421 seconds ( km/s) Burn time: 165 335 seconds (2 burns) Fuel: LH₂ / LOX Manufacturer: Douglas Aircraft Company Apollo Command Module (CM) ~~~~~~~~~~~~~~~~~~~~~ Height: 3.5 m (11.4 ft) Diameter: 3.9 m (12.8 ft) Mass: 5,560 kg (12,250 lb) Interior volume: 5.9 m³ (210 cu ft) Crew capacity: 3 Reaction Control System thrusters: 12 RCS thrust, ea.: 410 N (93 lbf) RCS fuel: MMH / N₂O₄ Manufacturer: North American Aviation / North American Rockwell Apollo Service Module (SM) ~~~~~~~~~~~~~~~~~~~ Height: 7.6 m (24.8 ft) Diameter: 3.9 m (12.8 ft) Mass: 24,520 kg (54,060 lb) Service Propulsion System engine: 1 Rocketdyne AJ10-137 SPS thrust: 91 kN (20,500 lb) SPS fuel: Aerozine 50 (50:50 mix of hydrazine/UDMH) / N₂O₄ Reaction Control System thrusters: 4 x 4 (16) Marquardt R-4D RCS thrust, ea.: 440 N (100 lbf) RCS fuel: MMH / N₂O₄ Manufacturer: North American Aviation / North American Rockwell Lunar Module (LM) ~~~~~~~~~~~~~ Height: m (23 ft 1 in) Diameter: m (13 ft 10 in) without landing gear Width: 9.4 m (31 ft) landing gear deployed Dry mass: 4,280 kg (9,430 lb) Launch mass: 15,200 kg (33,500 lb) Crew cabin volume: 6.7 m³ (235 cu ft) Habitable volume: 4.5 m³ (160 cu ft) Crew capacity: 2 Descent Propulsion System engine: 1 TRW LMDE DPS thrust: kN (10,125 lbf), throttleable DPS fuel: Aerozine 50 (50:50 mix of hydrazine/UDMH) / N₂O₄ Ascent Propulsion System engine: 1 Bell / Rocketdyne LMAE APS thrust: 16 kN (3,500 pounds-force), fixed APS thrust-to-weight ratio: APS fuel: Aerozine 50 (50:50 mix of hydrazine/UDMH) / N₂O₄ Reaction Control System thrusters: 4 x 4 (16) Marquardt R-4D RCS thrust, ea.: 440 N (100 lbf) RCS fuel: MMH / N₂O₄ Manufacturer: Grumman Aircraft 👀 Check out “SpaceWeek“, my weekly summary of all things space! 🔊 SpaceWeek is also available as an audio podcast on Libsyn, Apple Podcasts, Amazon Music/Audible, Samsung, iHeartRadio, Spotify, Audacy, Player FM, and others! 🌎 Come hang out in our 24/7 Satellite Time Lapse music stream, featuring gorgeous views of Earth from geostationary orbit! 📆 Raw Space's calendar of launches and events: 🗨 Join us on Discord for text and voice chat! 🚗 Interested in buying a Tesla? Use my referral code for 1000 miles of free Supercharging! 🤗 Thank you!
