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2. List of NASA's flight control positions - Wikipedia

   en.wikipedia.org/wiki/List_of_NASA's_flight...

   Landing support officer (LSO) team – maintained the airspace at any landing site, dispatch Search and Rescue teams if needed, act as first liaison in case of a landing outside the US; Nav support team – responsible for maintaining the on-board navigation (telemetry) and the ground navigation (tracking)

3. Apollo Guidance Computer - Wikipedia

   en.wikipedia.org/wiki/Apollo_Guidance_Computer

   The Apollo Guidance Computer (AGC) was a digital computer produced for the Apollo program that was installed on board each Apollo command module (CM) and Apollo Lunar Module (LM). The AGC provided computation and electronic interfaces for guidance, navigation, and control of the spacecraft. [ 3 ]

4. Launch Control Center - Wikipedia

   en.wikipedia.org/wiki/Launch_Control_Center

   LCC has conducted launches since the unmanned Apollo 4 (Apollo-Saturn 501) launch on November 9, 1967. LCC's first launch with a human crew was Apollo 8 on December 21, 1968. NASA's Space Shuttle program also used LCC. NASA has renovated the center for Space Launch System (SLS) missions, which began in 2022 with Artemis 1.

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6. AOL Live Support Plus

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   AOL Live Support Plus includes our top-of-the-line support and security products that will help protect your identity and information online. Get started today! Support when you need it: 24x7 Live Support gives you access to AOL experts over the phone or online chat, 24 hours a day, 7 days a week. Our experts are ready to assist you with any of ...

7. Unified S-band - Wikipedia

   en.wikipedia.org/wiki/Unified_S-band

   Apollo 15 Lunar Module and Lunar Roving Vehicle, August 1, 1971.The S-band dish antenna for the rover is visible. The Unified S-band (USB) system is a tracking and communication system developed for the Apollo program by NASA and the Jet Propulsion Laboratory (JPL).

8. Apollo command and service module - Wikipedia

   en.wikipedia.org/wiki/Apollo_command_and_service...

   The CSMs launched in orbit on Saturn IB ranged from 32,558 pounds (14,768 kg) (Apollo–Soyuz), to 46,000 pounds (21,000 kg) (Skylab 4). The omnidirectional antennas sufficed for ground communications during the Earth orbital missions, so the high-gain S-band antenna on the SM was omitted from Apollo 1, Apollo 7, and the three Skylab flights.

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