The Space Shuttle fleet has been flying now for about 25 years. In that time, there have been, unfortunately, two losses of crew and craft. Without question, both could have been prevented. A good number of folks – in government and not – combine that record with the cost of flying the shuttle and question why we continue to fly it. They also look at NASA’s post-Columbia culture and see numerous delays and safety-related scrubs and claim that the shuttle fleet is unsafe, unreliable, and generally wasteful. If you look at the direct costs involved with each launch, the shuttle costs about $60 million for each launch.
The initial contract for the Shuttle program was awarded early in the 1970’s. Construction on the first Shuttle airframe, Enterprise, began in June 1974. Designs for the vehicle had been in development since the late 60’s. Yeah – that’s right: the 60’s. We’re flying to space in a vehicle whose basic design is nearly 40 years old. The technology is, of course, quite a bit newer. Instruments and equipment have been upgraded and the airframe modified where necessary.
The design lifetime for each orbiter is 100 flights. Discovery, first launched in 1984, has recorded 32 flights. Atlantis has done 27 since its first flight in 1985. Endeavor, the newest, has done 19 since 1992. If the airframes are capable of really lasting to their design life, there is easily a lot of life left in the fleet.
Discovery is due for retirement in 2010.
Atlantis is due for retirement in 2008.
Endeavor is due for retirement in 2010.
Basically, they’re just being kept around to haul up pieces for the International Space Station and people to put them together. So, you might be asking, what then? What will, as our good President Bush has tasked us to do, take us to the moon and to Mars? Answer: the Orion. Think overgrown Apollo. Sort of.
Orion is basically two vehicle systems. There is a two-stage booster to lift a crew module (CM) and a service module (SM). The lift vehicle for this stack is called the Aries I. For a first stage, it will use a 5-segment solid booster derived from that currently used on the Shuttle. The second stage will be powered by an Apollo-derived J2X engine fuelled with liquid hydrogen (LH2) and liquid oxygen (LOX). While the solid booster may be recovered, the second stage is a throw-away.
The service module will provide propulsion, power and life support to the crew module. Only the CM returns to Earth. All of the equipment in the SM – an engine, solar cells, life support equipment – burns up in our atmosphere. Since the vehicle will be solar powered, there is no need for fuel cells (hydrogen + oxygen = electricity and water). However, this isn’t the savings it seems: no water out of the fuel cells means that every drop of water that goes will have to be carried along and recycled. The CM will parachute back to the surface, this time on land rather than sea as the Mercury, Gemini and Apollo missions did. I guess you have to have something to differentiate.
Notice that there is no lunar lander mentioned above. If you go to the moon, you need a lander. That will be launched in the Aries V. It will be powered by 5 RS-68 engines fueled with LOX and LH2 assisted by two solid boosters. It has a second stage similar to the Aries I.
Let’s tally. For a moon mission, you’ll be using 3 solid boosters, 5 RS-68 engines, 2 J2x engines, a Delta II-derived second stage engine on the SM. That’s just engines. You’ve also got tons of stuff that doesn’t ever come back. You can’t inspect things that failed. They’re gone.
A few facts.
The projected design life of the CM is 10 flights. It has an ablative heat shield that must be replaced after each flight.
The Shuttle was designed for 100 flights. It has a ceramic tile heat shield that is inspected with tiles replaced as necessary.
Each of the RS-68 engines is projected to cost $20 million. That’s $100 million for each launch.
The Shuttle’s engines cost $50 million each. They are designed to last 30 flights. That works out to $450 million for 90 flights. The engines are torn down, inspected and repaired after each flight.
The Orion CM is projected to accommodate 6 crew in about 545 cubic feet of space in one area. It is about 2.5 times larger than the Apollo CM.
The Shuttle has 2,325 cubic feet of space spread essentially over two decks and can accommodate 7. And that is with the airlock inside. Move it to the cargo bay and you’ve got 2,625 cubic feet. It also can carry 53,000 lbs to low Earth orbit in a cargo space 15 feet wide and 60 feet long. Then it can play with it using a robotic arm.
The Orion has no airlock. And no cargo capability.
The longest Apollo mission was just over 12 and a half days in duration.
The Shuttle’s longest mission was just over 17 and a half. 13 day flights are routine.
I don’t know that the shuttle could get us to the moon, but I’d like to believe that with a bit of Yankee ingenuity, it could. It could carry a lunar lander in the cargo bay with, I presume, enough room for the extra fuel required to perform a trans-lunar flight. And I don’t know about you, but I wouldn’t want to spend two weeks crammed into a tin can with 5 other people while traveling to anywhere. Longer missions are also possible with the shuttle; currently, Endeavor is undergoing a refit to allow extra provisions to be “jacked” into its current systems.
So let’s build 4 or 5 new shuttles using all that we’ve learned in the last 30 years and take them to the moon. The basic design appears to be as sound today as it was 40 years ago. Orion is just a step backward. That’s my take boys and girls. What’s yours?