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Originally posted by weedwhacker
I'm seeing a simularity in this Zorgon's post to things I've seen on YouTube...a haven, might I say, for morons. Unlike ATS, which attracts educated people.
Simularities include, but are not limited to: silly assertions, bad science, and, worst of all, horrible spelling and/or grammar.
Dear Zorgon,
I don't insult.... being new to this, then I apologize.
Stop getting your knowledge from movies like Armageddon and get a clue about how real spaceflight works - launching a space shuttle is just about the most complicated thing humans have ever done.
Flight Control System Push Button Indicators
These indicators are located on panel F2 for the commander and panel F4 for the pilot. The flight control system's push button light indicators transmit flight crew moding requests to the digital autopilot in the flight control software and reflect selection by illuminating the effective DAP state.
The push button light indicators are used to command and reflect the status of the pitch control mode. The pitch and roll/yaw indicators transmit moding requests to the digital autopilot and indicate the effective state of the pitch, roll and yaw DAP channels by lighting.
Auto indicates that control is automatic and no crew inputs are required. CSS is control stick steering; crew inputs are required but are smoothed by the DAP (stability augmentation, turn coordination)
Originally posted by johnlear
Yes, launching is a busy time but as far as the operation or flying of the shuttle I believe everything is automatic including the docking.
Originally posted by johnlear
Flight Control System Push Button Indicators
These indicators are located on panel F2 for the commander and panel F4 for the pilot. The flight control system's push button light indicators transmit flight crew moding requests to the digital autopilot in the flight control software and reflect selection by illuminating the effective DAP state.
The DAP is used mostly for rendezvous (NOT docking) burns where it is impossible for a human to fly the spacecraft e.g. exacting deorbit burns, MECO to OPS 2 transitions, etc.
Originally posted by dznetworks
Ever notice that shuttle launches always happen at an odd time never on the hour?
The beta angle is the angle between the orbital plane and a line drawn from the Sun to the Earth. As the beta angle increases, the ISS is exposed to more sunlight per orbit, and eventually it will be in constant sunlight -- in other words, there is no passing into the Earth's shadow for extended periods of time. This can create thermal problems, so special attitudes are chosen to counter these effects. The shuttle also has thermal constraints under these conditions. Since the attitude requirements of the ISS and shuttle would conflict when docked, shuttle/ISS flights are scheduled to avoid periods when the beta angle exceeds 60 degrees.
Hello, Capt Lear
I could not resist asking...have you ever flown an airplane that was certified for, or have you also been certified for, CATIII ops? CAT IIIa, CAT IIIb or CAT IIIc?
The reason I ask, not to put you on the spot...the L1011, as far as I know. was never certified for AutoLand. Nor were the B727, the DC-10, the DC-9 nor MD-80.
I have been trained to Cat III standards. Just thought you should know.
Respect.
The beta angle is the angle between the orbital plane and a line drawn from the Sun to the Earth. As the beta angle increases, the ISS is exposed to more sunlight per orbit, and eventually it will be in constant sunlight -- in other words, there is no passing into the Earth's shadow for extended periods of time. This can create thermal problems, so special attitudes are chosen to counter these effects. The shuttle also has thermal constraints under these conditions. Since the attitude requirements of the ISS and shuttle would conflict when docked, shuttle/ISS flights are scheduled to avoid periods when the beta angle exceeds 60 degrees.
Originally posted by johnlear
Thanks for the post 1553B. I was just wondering if the sun puts out heat in space why did the crew of Apollo 13 nearly freeze to death?
Hi John
Just wanted to say thanks for the L-1011 post. It´s been my favourite airliner ever since I can remember, flew both Delta and Eastern ships. Your knowledge about this plane must be outstanding. Hope to hear more from you on the subject. (perhaps on a different thread?).
By the way, I came to know abovetopsecret because of you. I did not know you were a conspiracy master, but I knew you were a famous airman, and that one of the models that you flew was the L-1011. Being that aviation is my hobby and that I just admire the engineering and craftsmanship of Lockheed, the road led to you and to this forum.
Cheerio
Camilo
Keeping the heat balance inside the space vehicle was achieved with radiators. Once there was less heat produced inside the vehicle due to power failure (heard of that, John?), the temps went down.
Originally posted by johnlear
Thanks for the post BS, the information on the system you call "google" was extremely informative and helpful. I had no idea such a site existed.
So the sun doesn't produce any heat that would warm the spacecraft?