he was being friendly.Both are impressive rockets! . The massive VAB became a space-age hangar, capable of housing four complete Saturn V launch vehicles and Apollo spacecraft where they could be assembled and checked out. The S-IVB third stage would be used as the second stage for the C-IB, which would serve both to demonstrate proof of concept and feasibility for the C-5, but would also provide flight data critical to development of the C-5.The C-5 was confirmed as NASA's choice for the Apollo program in early 1963, and was named the Saturn V.Before they moved under NASA's jurisdiction, von Braun's team had already begun work on improving the thrust, creating a less complex operating system, and designing better mechanical systems.The Saturn V's final design had several key features. I have a feeling the BFR is going to be the cargo launcher for all the needed supplies for Mars.The astronauts may still get to LEO via the F9/F9 Heavy for the trip to Mars.SX is working on a new rocket motor for this BFR, “The Raptor” which is a methane/liquid oxygen rocket.
The first extravehicular activity began at 11:59 a.m. April 21, after
It was agreed that the propulsion system should have a hover capability near the lunar surface but that this requirement also needed more study. (This meeting, like the one held February 13-15, was part of a continuing effort to select the lunar mission mode).Milton W. Rosen, NASA Office of Manned Space Flight Director of Launch Vehicles and Propulsion, recommended that the S-IVB stage be designed specifically as the third stage of the Saturn C-5 and that the C-5 be designed specifically for the manned lunar landing using the lunar orbit rendezvous technique. up to 183.5 kilometers away from it during the six-and-one-half-hour
This had the first mention of a 1,500,000 lbf booster (Juno V, later Saturn I). Despite some controversy, a Early in the planning process, NASA considered three methods for the Moon mission: At first, NASA dismissed LOR as a riskier option, as a The Saturn V's size and payload capacity dwarfed all other previous rockets successfully flown at that time. Phillips was confident the launch vehicle would have adequate payload capability, since Saturn V performance continued to exceed spacecraft requirements.
Record-setting temperatures every day all across the country has to mean something.Hi Dave, I agree wholeheartedly. Using the S-II had several advantages. X-ray spectrometer data indicated richer abundance of aluminum in the highlands, especially on the far side, but greater concentrations of magnesium in the maria. The total distance traveled in the lunar roving vehicle was
Throughout the initial planning, Presidential decision, and landing mode debate for the Apollo lunar landing goal, a variety of Saturn and Nova configurations were considered.
Other activities during the
26.7 kilometers. The 56-minute TV transmission showed excellent color pictures of the CSM, the intravehicular transfer, the LM interior, the earth, and the moon.At 10:47 p.m. EST, November 17, the spacecraft entered a lunar orbit of 312.6 x 115.9 kilometers. Voice communications should be provided from the earth to the lunar surface and the possibility of television coverage would be considered. During the return trip the astronauts made star-lunar landmark sightings, star-earth horizon navigation sightings, and live television transmissions.Studies were being conducted to determine the feasibility of intentionally impacting an S-IVB stage and an empty LM stage on the lunar surface after jettison, to gather geological data and enhance the scientific return of the seismology experiment. handrails, taking photographs, and describing rain squalls over KSC.
Apollo Program Director Samuel C. Phillips sent a message to the manned space flight Centers indicating that he wanted to supplement the findings of the S-IVB Accident Investigation Board with a review by the Crew Safety Panel of the possible impact on manned Apollo flights. He added that the issue must be resolved in order to finalize the AS-501 attitude maneuver and venting timeline.Apollo Program Director Samuel C. Phillips told NASA Associate Administrator for Manned Space Flight George E. Mueller that studies had been completed on the use of "direct translunar injection" (launch directly into a trajectory to the moon) as a mode of operation for lunar landing missions.
After the S-IVB was staged off the spacecraft following injection into the translunar trajectory, the service module would be used for midcourse corrections.
Phillips and a task force had started this study at North American November 22, 1965.Phillips added: "I am definitely not satisfied with the progress and outlook of either program and am convinced that the right actions now can result in substantial improvement of position in both programs in the relatively near future.
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