Title: Rapid Development of Space
1Rapid Development of Space
- Wayne Solomon
- August 2009
2Soviet Union scares the pants off.
- Sputnik 1 was first into low earth orbiting
satellite, 1957 - Plasma Density meas.
3Explorer I ( little tubesat that did..)
- US Enters Space, 1958, On Jupiter-C booster
- Located Van Allen
- Radiation belt, Launch
4To the Moon(practicing for Chicago)
- Soviets impacted the moon in 1959
- Luna 2
- Luna 3 returned
- photos from
- Moon in 1960 (where are pics!)
5Early US Missions to Moon (good try, but no
cigar)
- A number of attempts to impact the moon starting
with Ranger Series in 1964 - Atlas/Agena launcher
6U.S. Surveyor Program 1966, pad prints for
Apollo
- Seven Surveyor Vehicles were flown by 1968.
Five were successful, Atlas/Centaur Launch
vehicle - Exploring landing sites and technology, and
geoscience for Apollo program. - Turnaround in Space Race with Soviets and showed
that efforts were essentially tied.
7US Lunar Prospector (Return after 25 years,
better, faster, less for less)
- Search for water in 1998 with very low cost
Athena (three stage solid!) launcher. No H2O in
sight
8Lunar Prospector (Admit it, they tried some neat
stuff..)
- Gamma Ray Spectrometer..GeoChem
- Neutron Spectrometer.. Water (ice) signature
- Alpha Particle Spec.. Radon from volcano (?)
- Doppler Gravity.. Lunar gravity
- Magnetometer.. Local field
9Prospector (a big parking lot..)
10Soviet Lunar missions (lots of big iron out
there)
- Zond Series of failures before circumlunar probe
in 1968. Stripped down Soyuz SC.
11Chinese Lunar Explorer, years later,(slow and
steady)
- Chinese Lunar mission launch, 1997
- Mapping, impact data
12Oh my darling Clementine
- Clementine was a joint project between the
Strategic Defense Initiative Organization and
NASA, 1994. The objective of the mission was to
test sensors and spacecraft components under
extended exposure to the space environment and to
make scientific observations of the Moon and the
near-Earth asteroid 1620 Geographos
13Soviet Mars Orbiters, 1962-73 (lots more big
iron, later)
- Mars 2 and Mars 3 employed heavy Proton booster
- Like many earlier Mars missions they reached
destination but ended poorly - Some grainy Photos for their trouble!
- Better results on later missions
14U.S. Viking Program (JPL Mars scoop!)
- JPL Orbiters for survey and com. Relay with
lander, 1976 - Landers had N2O4/MMH thrusters for control and
propulsion. - Very successful effort.
- Launcher Titan III
- centaur vehicle
15Mars Pathfinder, 1996,(Oh, to be a Bot, oops
mighty big rock)
- First of a series of JPL Mars missions that
included the first successful rover
16Mars Global Surveyor, 1996-2006 (Serious
exploration stuff)
- Launch with package of cameras and instruments to
provide maps for landers
17Cassini Spacecraft, 2004,( A quick peek at the
Saturn, lots more similar stuff later..)
- Tracking storms on Saturn. Storms last for
months at a location called Storm Alley
18Orbview 2 (In the looking glass..)
- Launched in 1997 is early earth imaging circular
sun synchronous satellite to study Oceans on a
routine basis. Ocean conditions for fishing,
climate change, etc.
19TSX-5 ( not sure why)
- A 2000 launch, Low earth orbit small satellite
with 68 degree inclination for Air Force
environmental . Research., imaging, etc.
20Intelsat16 ( Communications Sats cover the globe)
- Geo Communications Satellite, to launch in 2010
from Baikonur Cosmodrome, Kazakhstan. 24 Ku-band
transponders
21NSS-9 (what can I say)
- Orbis Netherland C-band Satellite for 28
transponders which can be linked with three beams
for full earth coverage. 5000 lb with Power 2.3
Kw, 3 axis stabilized. - Arian-V launcher, 2009
22Defense Support DSP, Imaging Satellite (ICBM
watch from GEO)
- Last generation of DSP SatellitesThe satellites
are in geosynchronous orbits, and are equipped
with infrared sensors operating through a
wide-angle Schmidt telescope. The entire
satellite spins 1 so that the linear sensor
array in the focal plane scans over the earth six
times every minute. Typically, DSP satellites
were launched on Titan IVB boosters with Inertial
Upper Stages. The last one (flight 23) was
launched in 2007 aboard the first operational
flight of the Delta IV Heavy rocket, as the Titan
IV had been retired in 2005. All 23 satellites
were built by prime contractor Northrop Grumman
Space Technology, formerly TRW, in Redondo Beach,
CA.
23Another View of DSP
- Current launch detection from Geo.
24Next generation EO/ IR imaging (Cost overrun,so.)
- Launch failure has led to new requirements for
next generation imaging systems
25Radar Imagery, (Sherlock Holmes..)
- NROs future radar imaging satellite
26EOS Weather Satellite, 1994, The farmers love
it, me too..
- GOES Series major weather information for N.
America From GEO - EU, Russ, China, Japan, India have world pretty
much covered from GEO
27GEOS Series, 1994
- NOAA placed three axis stabilized series in GEO
- Vis/IR Spin scan radiometer day and night
observation along with interval imagery - Monitoring water vapor
28Polar Orbiting Weather, (the really big
picture)G. Davis, 2007)
- Several Series, Several DoD versions starting
late 50s. NASA and NOAA intitiated sun
synchronous Tyros weather Satellites in early
60s,Nimbus series (mid 60s) - Visible and infrared scanning radiaometers
- NOAA Partners with EUMETSAT for full time
coverage (day and night) with new vehicles to
contain.(next slide please!)
29Polar Orbiting Weather(G. Davis, 2007), details,
details
- Third Generation Advanced Very High Resolution
Radiometer - (AVHRR/3) A six-channel imaging radiometer to
detect energy in the visible and IR. High
Resolution Infrared Radiation Sounders (HIRS/4) - multispectral atmospheric sounding instrument to
measure IR scene radiance. - . Advanced Microwave Sounding Unit (AMSU-A) A
cross-track scanning total power Microwave
radiometer to measure scene radiance. - . Search and Rescue Satellite-Aided Tracking
(SARSAT) Instruments - Others
30IKONOS, 2000, (Google maps??)
- Commercial Satellite high resolution imagery, 1m
pancromatic and 4 m multispectral - Polar sunsynchronous orbit
- 3 axis stabilized with four reaction wheels
- LM900 bus (Iridium)
31Arian V (Each version just keeps getting bigger..)
- Ariane 5 is a European expendable launch system
designed to deliver payloads into geostationary
transfer orbit or low Earth orbit - No. solid boosters2Engines1 SolidThrust 6,470 kN
(1,450,000 lbf) Specific impulse275 s Burn
time129 sec - VulcainThrust1,114 kN (250,000 lbf)Specific
impulse430 s Burn time589 secondsFuelLH2/LOX
32Components Ariane 5 (bits and pieces!)
Ariane 5 ECB was planned to have an ESC-B upper
stage using a new Vinci expander cycle type
engine. The GTO capacity is to increase from 8000
kg to 12,000 kg
33Chinese Progress (Lots of early trouble but U.S
companies fixed)
- Long March 2E launch in 1990
- Long March 3C launch in 1996
- Space Launch Vehicles including
- Moon Probe in 2007
34Chinese Family of Space Long March Launchers, (
No Foreign technology here!)
- Employ Storable lower stages and Hydrogen Oxygen
upper Stages
2D
2F
3C
4C
35Dongfanghong(DFH-3),1997 (more me too..)
- General class of Chinese communications
satellites with common bus
36ZiYaun-1,1999 (Join the green croud?)
- Earth resources Satellite and later series on
CZ-4 launcher, joint with Brazil - Payload 5-band ccd camera 4-band infrared
multi-spectrum scanner 2-band broad
field-of-view imaging instrument.
37Fenyung Metrological Satellite Series, 2008,( not
sure what this adds..)
- Spin Stabilized multispectral GEO satellite.
- Several earlier variants were only partially
successful. - Vis-IR
38Beidou Navigation Series, 2000 (Chinese military
gps version..)
- Experimental group in GEO and a number of Medium
orbit navigation Satellites - Accuracy to 10 meters
39Chinese Ballistic Missile
- First Solid Rocket boosters, DF-21, 1986
- Low yield nuclear, 60 deployed in 1991
40Communications and Navigation
41Commercial/Dual Purpose
42Global Positioning, GPS, (no more excuses for
being late..)
- US Owned Utility operated by Air Force for
military and commercial navigation - 24 Satellites transmitting position and time
- Worldwide monitor and control ground stations
- User systems which calculate 3D positioning
433D Spatial and time Peter Dana, Univ of Texas
- Information from four satellites in view
- GPS provides specially coded satellite signals
that can be processed in a GPS receiver, enabling
the receiver to compute position, velocity and
time.
44A View of Constellation (cover the planet, baby..)
45Orbital Coverage, (The common bus.)
- The orbit altitude is such that the satellites
repeat the same track and configuration over any
point approximately each 24 hours (4 minutes
earlier each day). - There are six orbital planes (with nominally four
SCs in each), equally spaced (60 degrees apart),
and inclined at about fifty-five degrees with
respect to the equatorial plane. - This constellation provides the user with between
five and eight SCs visible from any point on the
earth.
46Ground Tracks (notice our new flat world..)
47Control (distributed control anyone? ..)
- GPS Master and Monitor Net
48GPS Navigation (Its so, simple)
- The Master Control facility is located at
Schriever Air Force Base in Colorado. Monitor
stations measure signals from the SCs which are
incorporated into orbital models for each. - The models compute precise orbital data
(ephemeris) and SC clock corrections for each
satellite. The Master Control station uploads
ephemeris and clock data to the SCs. The SCs then
send subsets of the orbital ephemeris data to GPS
receivers within view.
49Users/Military (targeting, etc..)
- Authorized users with cryptographic equipment and
keys and specially equipped receivers use the
Precise Positioning System. (military) - PPS Predictable Accuracy
- 22 meter Horizontal accuracy
- 27.7 meter vertical accuracy
- 200 nanosecond time accuracy
50Users/Civilian (Easy stuff..)
- The SPS accuracy is intentionally degraded by the
DOD by the use of Selective Availability. - SPS Predictable Accuracy
- 100 meter horizontal accuracy
- 156 meter vertical accuracy
- 340 nanoseconds time accuracy
51Navigation ( ah, the gory details..)
- The GPS Navigation Message consists of
time-tagged data bits marking the time of
transmission of each subframe at the time they
are transmitted by the SC. A data bit frame
consists of 1500 bits divided into five 300-bit
subframes. - A data frame is transmitted every thirty seconds.
- Three six-second subframes contain orbital and
clock data. - SC Clock corrections are sent in subframe one
- precise SC orbital data sets (ephemeris data
parameters) for the transmitting SC are sent in
subframes two and three. .
52SatCom (Ships at sea, etc..)
- Early Navy sat com bounced teletype off the moon
(1950s, first sat com) to contact ships at sea. - Navy then went to analogue hf (high frequency)
transmission earth-to-satellite-to-earth for
nearly 50 years. - Now, communications are pretty much all digital
53DSCS III, (Typical antenna farm..)
54SatCom (Ships at sea..)
- The two types of communications are ACTIVE and
PASSIVE. A passive satellite only reflects
received radio signals back to earth. An active
satellite acts as a AMPLIFIER/REPEATER
55Coverage (earthy orbits)
- The inclination of the orbit determines the area
covered by the path of the satellite. The greater
the inclination, the greater the amount of
surface area covered by the satellite - A satellite in a circular orbit from
approximately 2,000 miles to 12,000 miles above
the earth is considered to be in a MEDIUM
ALTITUDE ORBIT.
56Synchronous Orbit (Ah, so far away, but..)
- A satellite in a circular orbit at a height of
approximately 19,300 nautical miles above the
earth is in a synchronous orbit.
57Coverage from DSCS Birds
58DSCS Satellite (Navy, 1980s- 2000s..)
- Picture shows each pair of transmit and receive
dish antennas. As you can see, a large area of
the earth can be covered using only one
satellite, in geo. - Newer communications satellites have about 32,000
solar cells mounted on the surface of the
satellite, and they supply about 520 watts. A
nickel cadmium battery is used for backup power
during eclipses. - The latest versions of communications satellites
use a stationary platform with four high-gain
antennas. Two steerable narrow beam antennas are
used for communications between and within
regions of high traffic density. Two horn
antennas provide for earth communications between
facilities outside the narrow beam coverage.
59Iridium, 1997 (Motorola dream)
- The Iridium satellite constellation is a large
group of satellites used to provide voice and
data coverage to satellite phones, pagers and
integrated transceivers over Earth's entire
surface. - Iridium Satellite LLC owns and operates the
constellation and sells equipment and access to
its services. The constellation requires 66
active satellites in orbit to complete its
constellation and additional spare satellites are
kept in-orbit to serve in case of failure.1
Satellites are in low Earth orbit at a height of
approximately 485 mi (781 km) and inclination of
86.4.