Slide 65(a) of 99
When the International Space Station plans were finalized in 1993/94, NASA was very concerned about the high cost of resupplying ISS using the agency's ageing Space Shuttle fleet. The cost of seven Shuttle was then estimated to be $2.8 billion, or $90,000+ per kilogram of useful payload to ISS! Consequently NASA started a highly touted research program in 1994 to develop a radically cheaper fully reusable single-stage-to-orbit spaceplane to replace the Shuttle. Private industry was supposed to pay for and operate the SSTO after the NASA-financed subscale "X-33" program had demonstrated the required technologies by the turn of the century.
Today, the solution to the ISS transportation problem isn't as obvious, though. Lockheed-Martin's "Venturestar" X-33 design was chosen by NASA in 1996, but the company has been unable to develop the vehicle on time and on budget. At the same time as fully reusable SSTO appears to be a more challenging goal than previously thought, the cost of a Space Shuttle launch has fallen in recent years thanks to partial privatization of the day to day operations. Vehicle upgrades such as the new super-lightweight external propellant tank + a more efficient Multi-Purpose Logistics Module have also increased the Shuttle's payload capability by almost 200%. The United Space Alliance has offered to fly five annual ISS resupply missions for just $1.5 billion provided NASA agrees to certain reforms (=further privatization of the Shuttle program, standardized ISS mission format, no day-to-day NASA oversight, permission to offer 1-2 "surplus to requirements" Shuttle flights/year to commercial customers). The cost to NASA would thus be about $35,000/kg of useful payload delivered to ISS. Not cheap by any stretch of the imagination but still surprisingly competitive vs. future systems, when development costs are factored in.
It thus appears the Space Shuttle will be around for quite some time. The Shuttle does meet
the basic requirements of reasonably regular delivery & return of crews, experiments and
supplies. But it is not capable of increasing launch rate or launching on demand, and the
Shuttle does not really provide high reliability for delivery & return of high-valued
cargo and crew. Another significant shortcoming is 30-50% of all Space Station users would
like to have access to their payload as late as 10 hours before launch and as early as 2 hours
after landing, according to the 1993 COMMERCIAL SPACE TRANSPORTATION STUDY (CSTS) report. The Shuttle
is not as affordable or flexible as ISS users would like, e.g. only 30% of the payload racks
provide thermal control.
As noted earlier, NASA originally anticipated about seven ISS crew transfer & resupply missions
per year == ~30 metric tons of cargo. The expected U.S. transportation requirement is now about
43 metric tons, in part because the Russians will be unable to launch as many Progress cargo
craft as planned. The CSTS report assumed the number of flights would change little even if
a low-cost launch vehicle were available; the resulting savings probably wouldn't be invested
in additional ISS upgrades since the program already is over budget. NASA would, at most, be
allowed to fly 1-2 additional missions per year to increase the ISS science output. This is
the "high probability scenario" shown in the table below.
These scenarios assume each kilogram of ISS payload will cost $22,000
to produce on average (=scientific equipment is ten times more expensive
but food and clothes obviously cost far less). Cheaper space transportation
would permit NASA to invest some of the savings in additional experiments
and equipment to increase the output of the Station. Thus, the low-probability
CSTS scenario assumed 80% of the funds saved thanks to cheaper space transportation
would go into Space Station additions/upgrades. For the medium probability scenario,
20% of the savings would be used for Space Station growth. Since crew time is one
of the most important limiting factors, any ISS expansion program probably would
have to start by adding more habitation & laboratory modules. The CSTS parametric
growth estimates of the U.S. hab & lab modules are:
The "high growth" scenario may well include additional developments
such as assembly of large manned lunar or Mars mission spacecraft at
or near the Space Station; this could increase the annual transportation
requirement to 500-1,500 metric tons per year! The Station's scientific
capabilities would also be enhanced if some sensitive processes were moved
to separate man-tended free-flying platforms. This would also allow other
ISS users to have frequent access to the main ISS complex without disturbing
sensitive microgravity experiments. NASA's current plan (below) calls for two
30-day periods of undisturbed microgravity work every 92 days.
FUTURE SPACE STATION GROWTH AND NEW SPACE TRANSPORTATION OPPORTUNITIES
ANNUAL U.S. PAYLOAD TO SPACE STATION (4250kg payload/flight)
Option Scenario
1993 transp. cost (~$94K/kg)
1/10th (=$9400/kg)
1/100th (=$940/kg)
High Probability
29,750kg
31,875kg
31,875kg
Medium Probability
34,000kg
48,875kg
55,250kg
Low Probability
38,250kg
68,000kg
80,750kg
=ANNUAL U.S. ISS PAYLOAD PRODUCTION COST (@ $22,000/kg)
Option Scenario
1993 transp. cost (~$94K/kg)
1/10th (=$9400/kg)
1/100th (=$940/kg)
High Probability
$655M
$701M
$701M
Medium Probability
$748M
$1,075M
$1,216M
Low Probability
$842M
$1,496M
$1,777M
=TOTAL ANNUAL U.S. ISS TRANSPORTATION COST
Option Scenario
1993 transp. cost (~$94K/kg)
1/10th (=$9400/kg)
1/100th (=$940/kg)
High Probability
$2,800M
$300M
$30M
Medium Probability
$3,200M
$460M
$52M
Low Probability
$3,600M
$640M
$76M
Number of habs & labs
Crew
Crew available for experiments
Crew requirements (racks/yr.)
User requirements (racks/yr.)
Space Station (racks/yr.)
=Power required (kwatts.)
=Total upmass (kg)
1
4
2
17
17
15
30
29750kg
2
8
5
34
43
23
75
46750kg
3
12
8
51
68
30
120
63750kg
As noted previously, NASA initially identified a new fully reusable "single stage to orbit" spaceplane as its preferred solution to the ISS transportation problem. However, in 1999 the agency was forced to expand the number of alternate systems investigated for the Space Transportation Architecture Study. The vehicle configurations were:
The risk-to-reward ratio does not yet appear to be sufficiently good to warrant the $4 billion+ development cost of the reusable launch vehicle alternatives on the list. Thus, the best near term solution appears to be a combination of modest Shuttle upgrades+privatization as well as investment in an unmanned "backup" cargo transfer vehicle for the EELV. Since both EELV versions -- Boeing's Delta IV family and Lockheed-Martin's Atlas V -- will be competitors, it makes sense to outsource some unmanned Space Station resupply services on a "best bidder" basis too. Meanwhile, NASA needs to continue pursuing low cost reusable launch vehicle technologies and experimental vehicles to reduce the risk to the private sector. Eventually, a reusable equivalent of the EELV will make business sense but current launch markets are not yet sufficiently lucrative for it.