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1969 Apollo 11 TV Transmission from halfway to Moon,

🔴 Patreon:   / rawspace   👕 "Rawlmart" merch store: https://shop.rawspace.live 🔵 PayPal: https://paypal.me/RawSpaceVideos 👍 Like ✅ Subscribe 🔔 Activate Notifications On 17 July 1969, 1 day 9 hours and 59 minutes after Apollo 11 launched (33:59 GET or mission time, 11:31pm GMT), the crew sent this broadcast from 130,000 miles (209,215 km) away - about halfway to the moon. 1:48 Neil Armstrong describes their view of the Earth from 130,000 miles away. 13:27 Mike Collins and Neil Armstrong inside the Command Module, shot by Buzz Aldrin. 17:58 Buzz Aldrin explains the star charts they are using for navigation. 20:55 Buzz Aldrin does pushups in space. 22:17 Mike Collins demonstrates how they make chicken stew. 24:21 Mike Collins spins a flashlight in zero gravity. 26:40 Mike Collins describes where they sleep onboard the Command Module. Apollo 11 video playlist:    • Raw Space: 1969 Apollo 11 Moon Mission   Apollo 11 Technical Air-to-Ground Voice Transmission transcript: https://www.hq.nasa.gov/alsj/a11/a11t... Apollo 11 detailed timeline: https://history.nasa.gov/SP-4029/Apol... 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: 7.04 m (23 ft 1 in) Diameter: 4.22 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: 45.04 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: 19.44 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 by Raw Space   📆 Raw Space's calendar of launches and events: https://tiny.cc/RawSpaceSched 🗨 Join us on Discord for text and voice chat!   / discord   🚗 Interested in buying a Tesla? Use my referral code for 1000 miles of free Supercharging! https://ts.la/matthew76381 🤗 Thank you!