I've been an observer and sometime participant in the
microsatellite business since 1992,
when I wrote my first paper on the
topic. The field grows and changes so
fast it's very hard to keep up
with the basic news, let alone all the
accomplishments being logged. But where did it begin?
This is an intermittent series poking through some of the
information I (and some co-authors like Erika Vadnais) have picked up in many
years of looking at this topic, talking to the entrepreneurs and the engineers,
and writing. (Not included is information
I/we developed on company time at our employers’ expense: companies get touchy
about that.) However, as authors of The First Space Race (NASA/Texas A&;M, 2004) (which developed out of a microsat
history book project called Little Star, which we may actually get back to one
of these years) we learned lot on our own time: enough to provide some historical
context to a fast-moving industry.
We'll go back to the earliest days in later installments, but I wanted to focus this time on the decade that is easily forgotten but was absolutely pivotal: the 1990s.
First. what's a microsatellite? I like the common (but not universal)
standard of 100kg or less for a microsatellite and 10 kg or less for a
nanosatellite. Back in the 90s, the
U.S. Air Force (USAF) referred to “smallsats” as under 1,000kg or 500kg, either of which
is hopelessly antiquated after decades of shrinking electronics and other
components. For a long time it was
generally accepted a microsat would be single-string (no redundant components)
and single-mission, but relentless miniaturization is slowly moving us away
from those norms.
I’m going to focus in this first segment on military satellites,
because truly commercial microsatellites are a relatively recent
development. The pioneering Orbcomm UHF
constellation by Orbital Sciences Corporation (OSC) (which also flew the first small
booster developed in the U.S. in decades, the air-launched Pegasus) orbited its
first satellite, the pioneering Orbcomm-X (or Datacomm-X) in 1991, but Orbcomm
for many years had commercial microsats to itself.
To get back to the topic, the microsat didn't emerge out of nowhere.
The first
satellites, like America's pioneering Explorer I and Vanguard I of 1958, were
small because they had to be (and military because no one else had the money
and expertise). Explorer I, America’s
first response to the much larger Sputniks, was built into the fourth stage of
the Jupiter-C launch vehicle. The satellite portion was only 84 cm long and 15 cm in
diameter. This section was made of 410
stainless steel, its bare sandblasted surface marked with white stripes of
aluminum oxide. Explorer 1 weighed 6.35
kg on its own and 14 kg if the fourth stage of the booster (which remained
attached) was counted.
An Explorer 1 model with transparent display version of front section (NASA)
As boosters became more powerful from the early 1960s on, the
U.S. military moved to orbiting increasingly larger and more capable payloads.
In the decade from 1978 to 1987, for example, only six military microsats were
launched. (Four of these belonged to the
Navy’s Transit navigation series, which operated from 1962 through 1996.)
Beginning in 1987, the Defense Advanced
Projects Research Agency (DARPA) (known for part of its history as ARPA), led a
resurgence of interest which resulted in military proof-of-concept satellites of the late 80s and early 90s with clunky acronym-ed names like GLOMR, MACSAT, DARPASAT, LOSAT-X,
and the MicroSat constellation. The most notable one of the early 1990s was the
UHF store-and-forward communications bird called MACSAT, one of which was
pressed into operational use in the first Persian Gulf War. Despite this success, the Navy's proposal for
a follow-on constellation, ARCTICSAT, was canceled. For the rest of the decade,
the largest U.S. military space service, the USAF, basically laughed out loud
at the idea these toys could be useful.
(OK, an organization cannot physically laugh, but the Air Force came as
close as possible.)
Two MACSATs stacked for launch (DARPA)
NASA never abandoned microsats completely: the
Explorer series moved from its original Army home to NASA and continues today, and the Particles and Fields Subsatellite (PFS) series put tiny satellites into orbit around the Moon from Apollo missions. NASA entered a new era in 1995 when MicroLab-1
(later turned over to the contractor, OSC, and redesignated OrbView-1)
demonstrated that a microsat could provide environmental data. The 68-kg satellite mapped thunderstorm
activity and created moisture and temperature profiles by measuring the
occultation of Global Positioning System (GPS) signals received through the
atmosphere.
Military communications, as well as commercial telephone, broadcasting,
and other applications, was generally provided since the 1960s by large
high-capacity satellites in the geostationary belt. Microsats were not going to add much here,
but there’s another way to do commemorations. Low-orbiting satellites can receive
comm over a theater and downlink it to a headquarters and vice versa (store-and-forward)
or provide continuous “bent-pipe" communications with a constellation of
spacecraft to ensure that at least one satellite will always be in contact with
the user. Such smallsat constellations
were orbited by the U.S. and the former Soviet Union beginning in the
1960s. The concept was tested again by
DARPA in 1991 when a single launch vehicle orbited seven 23-kg UHF MicroSats,
creating a constellation providing continuous voice and data communication
within a footprint about 5000 km wide. The entire system, including launch,
cost under $20 million (M) in 1998 dollars.
After Congress denied DARPA requests for $30M in Fiscal Year
(FY) 1993 and $24M in FY 1994 requests for related projects, the DARPA
"lightsat" program was essentially dead. This was despite the 1994
Air University study Spacecast 2020, which made another point in favor of such
satellites. If a large satellite has a
nominal 10-year life and a microsat two years, the microsats are able to go through five generations of
technology improvement for every one generation of the largesat. This has become more important as time and
technology have progressed: every large satellite launched is essentially
behind the technology curve thanks to years in preparation. In 1998, Air Force Chief Scientist Daniel
Hastings gave a strong endorsement to "smallsats." While cautioning that “moving to smaller,
distributed satellites is not a panacea for all problems,” he said, “The
potential exists for really revolutionary changes in respect to moving to smaller
systems.” He had no idea how right he was.
Other countries made experiments in this decade, too, and
not only in communications. One of the
most interesting was France's 50-kg CERISE, launched in 1995. This spacecraft monitored HF emissions to
validate technology for a future operational signals intelligence microsat
called Clementine (no relation to the U.S. lunar probe of the same name.)
The commercial world didn’t lack for pioneering
entrepreneurs, but for quite a while Orbcomm was the only one that got serious
traction. One of the pioneering commercial firms, predating Orbital, was AeroAstro,
led by visionary/evangelist Rick Fleeter. Fleeter had no patience with
approaches that just tried to shrink conventional satellites a little. He once
observed that the military “thinks a small satellite is 900 kilograms. We think it’s 9.” AeroAstro tried to shrink satellites drastically
in the late 90s, marketing the 1-kg Bitsy spacecraft bus. It was advertised as costing under $100,000
(plus payload), being customizable for applications including remote sensing,
communications, space science, and technology testing, and taking nine months
from ordering to delivery to a launch pad.
The vision, though, as so often happens, was ahead of the market. Useful
payloads small enough and using only a few watts of electricity just were not
ready yet, except for UHF radios. No Bitsy ever flew.
One of the reasons microsats were dismissed in the 1990s was
their inability to take anything but very low-resolution images. This was considered a hard limit: the
relationship between mirror size and image resolution (equivalent to the pixel
size in electronic images) was inviolate. If you wanted a satellite that could
spot a car (much less read the proverbial license plate), you needed a mirror diameter
measured in meters. In the 1990s,
inventions like “folded optics” and the Charge Coupled Device (CCD) imager
began a revolution which would lead eventually to the Planet (formerly Planet
Labs) microsatellites in orbit today, in which images with three-meter resolution
are taken from a satellite with a once-ridiculous aperture diameter of
10cm.
Other advances drove miniaturization, including the
reduction of computers to single chips and composite-based construction. FORTE, a 215-kg satellite built by Los Alamos
and Sandia National Laboratories and launched in 1997 to watch for the
electromagnetic signatures of nuclear tests, flew the first frame made entirely
of graphite-epoxy composites. Compared
to an all-aluminum structure, this reduced the weight from 64 to 42 kg.
By the end of the 1990s, the microsatellite revolution,
despite halting and sometimes shaky progress, was advancing on a broad
front. Imaging, communications, electronic
intelligence, weather, and other proof of concept satellites had established
the potential utility of microsats, and the advance of technology – much of it in
the consumer electronics industry – was enabling leaps in capability. The stage was set for the real revolution –
one that would be permanent.
