report on project mercury
Apr. 22nd, 2011 08:32 pm
Found by my awesome housemate Matthew at the neighbor's garage sale: "Results of the Second United States Manned Orbital Space Flight" (or, big pdf).
I love that cover illustration.
In the hopes that this work may in some way contribute to their exploration of space, this is dedicated to the crew members of this country's present and future manned space programs. If only I could join them in their exciting endeavors!Six and a half years later, he walked on the moon.
The F-1 burned two short tons (1.8 t) of liquid oxygen (LOX) and one ton (0.9 t) of RP-1 (kerosene) each second generating over 1.5 million pounds-force (6.7 meganewtons) of thrust. During their two and a half minutes of operation, the five F-1s propelled the Saturn V vehicle to a height of 52 km (32 miles) and a speed of 8,700 km/h (5,400 mph). The combined propellant flow rate of the five F-1s in the Saturn V was 3580 U.S. gallons (13552 liters) per second. The flow rate could empty a 30,000 U.S. gallon (113,562 liter) swimming pool in 8.5 seconds. Each F-1 engine has more thrust than all three space shuttle main engines combined.I'm not quite sure what all the plumbing is about;