If you are not already a subscriber, you are welcome to enter your email address here to sign up to receive the Space History newsletter on a daily basis. Under no circumstances will we release your legitimate email address entered here to outside persons or organizations, and it will only be used for mailing the specific information you have requested.
Enter your email address here:
 
Unsubscribe instructions are included in every newsletter issue in case you decide you no longer wish to receive it.

Note: We record the IP address from which subscriptions are entered to help prevent SPAM abuses.


1838
Born, Count Ferdinand von Zeppelin, at Konstanz, Grand Duchy of Baden (now part of Baden-Württemberg, Germany), first large-scale builder of the rigid dirigibles which eventually became synonymous with his name
http://www.firstworldwar.com/bio/zeppelin.htm

1861
Died, Elisha Graves Otis inventor (safe elevator)

1938
H Alikoski discovered asteroid #2911.

1947
The largest sunspot ever observed was discovered, roughly 18 billion square km in area, an amazing 6,132 millionths of the visible solar disk.

1964 16:00:01 GMT
NASA launched the unmanned GT-1 test of the structural integrity of the Gemini spacecraft and compatibility of Gemini and the Titan II launch vehicle. The test was successful, recovery was not planned; it reentered after the 64th orbit and disintegrated.
Gemini 1 was an uncrewed orbital test of the Titan 2 launch vehicle, the Gemini spacecraft structural integrity, and the launch vehicle-spacecraft compatibility. The test covered all phases through the orbital insertion phase. Other objectives were to check out launch vehicle-spacecraft launch heating conditions, launch vehicle performance, launch vehicle flight control system switch-over circuits, launch vehicle orbit insertion accuracy, and the malfunction detection system. This was the first production Gemini spacecraft and launch vehicle.

The Gemini 1 launch took place on 8 April 1964 at 11:00:01 a.m. EST from Complex 19 at Cape Kennedy, Florida. Six minutes after launch, the Titan 2 booster placed the Gemini spacecraft and the attached second stage in a 160.5 x 320.6 km orbit with a period of 89.3 minutes. An excess speed of 22.5 km/hr sent the spacecraft 33.6 km higher than planned. Mission plans did not include separation of spacecraft from the 3.05 meter diameter, 5.8 meter long Titan stage 2, both orbited as a unit. The planned mission included only three orbits and ended about 4 hours 50 minutes after launch with the third pass over Cape Kennedy. The spacecraft was tracked until it reentered the atmosphere and disintegrated on the 64th orbital pass over the southern Atlantic on 12 April 1964. The systems functioned well within planned tolerances and the mission was deemed a successful test.


NASA photo
http://nssdc.gsfc.nasa.gov/database/MasterCatalog?sc=1964-018A

1966
NASA's OAO 1, the first orbiting astronomical observatory, was launched.

1967
USSR launched the unmanned Cosmos 154 satellite with orbital data similar to a manned flight. It was believed to be a possible precursor to a later Soyuz flight.

1971
A 6 pound meteorite struck the home of Robert and Wanda Donahue in Wethersfield, Connecticut.

1978
W Liller discovered asteroid #2449.

1993 01:29:00 EDT (GMT -4:00:00)
NASA launched STS 56 (Discovery 16, 54th Shuttle mission) carrying the ATLAS-2 and SPARTAN-201 experiment packages.
The first launch attempt of STS 56 on 6 April 1993 was halted at T-11 seconds by orbiter computers when instrumentation on the liquid hydrogen high point bleed valve in the main propulsion system indicated off instead of on. Later analysis indicated the valve was properly configured; 48 hour scrub turnaround procedures were then implemented. The final countdown on 8 April 1993 proceeded smoothly.

The primary payload for STS 56 was the second flight of the Atmospheric Laboratory for Applications and Science (ATLAS-2), designed to collect data on the relationship between the Sun's energy output and the Earth's middle atmosphere, and how these factors affect the ozone layer. It included six instruments mounted on a Spacelab pallet in the cargo bay, with the seventh mounted on the wall of the bay in two Get Away Special (GAS) canisters. Atmospheric instruments included the Atmospheric Trace Molecule Spectroscopy (ATMOS) experiment, the Millimeter Wave Atmospheric Sounder (MAS), and the Shuttle Solar Backscatter Ultraviolet/A (SSBUV/A) spectrometer (on the cargo bay wall). Solar science instruments were the Solar Spectrum Measurement (SOLSPEC) instrument, the Solar Ultraviolet Irradiance Monitor (SUSIM), and the Active Cavity Radiometer (ACR) and Solar Constant (SOLCON) experiments.

ATLAS-2 is one element of NASA's Mission to Planet Earth program. All seven ATLAS-2 instruments first flew on ATLAS-I during STS-45, and were scheduled to fly a third time in late 1994.

On 11 April, the crew used the remote manipulator arm to deploy the Shuttle Point Autonomous Research Tool for Astronomy-201 (SPARTAN-201), a free-flying science instrument platform designed to study velocity and acceleration of the Solar wind and observe the Sun's corona. Collected data was stored on tape for playback after return to Earth. SPARTAN-201 was retrieved on 13 April.

The crew also made numerous radio contacts to schools around the world using the Shuttle Amateur Radio Experiment II (SAREX II), including brief radio contact with the Russian Mir space station, the first such contact between Shuttle and Mir using amateur radio equipment.

The other cargo bay payload was the Solar Ultraviolet Experiment (SUVE), sponsored by Colorado Space Grant Consortium and located in a Get Away Special (GAS) canister on the cargo bay wall.

The middeck payloads were the Commercial Materials Dispersion Apparatus Instrumentation Technology Associates Experiment (CMIX), the Physiological and Anatomical Rodent Experiment (PARE), Space Tissue Loss (STL-1) experiment, the Cosmic Ray Effects and Activation Monitor (CREAM) experiment, the Hand-held, Earth-oriented, Real-time, Cooperative, User-friendly, Location-targeting and Environmental System (HERCULES), Radiation Monitoring Equipment III (RME III), and an Air Force Maui Optical Site (AMOS) calibration test.

STS 56 ended on 17 April 1993 when Discovery landed on Runway 33, Kennedy Space Center, Florida. Rollout distance: 9,530 feet (2,905 meters). Rollout time: 63 seconds. Mission duration: nine days, six hours, eight minutes, 24 seconds. Landed revolution 148. The landing originally set for 16 April at Kennedy Space Center was waved off due to weather.

The flight crew for STS 56 was: Kenneth D. Cameron, Commander; Stephen S. Oswald, Pilot; C. Michael Foale Ph.D., Mission Specialist 1; Kenneth D. Cockrell, Mission Specialist 2; Ellen Ochoa, Mission Specialist 3.

http://www-pao.ksc.nasa.gov/kscpao/chron/sts-56.htm

1997 14:33:11 EDT (GMT -4:00:00)
NASA's STS 83 (Columbia 22, 83rd Shuttle mission) landed early, the third shortened mission in the Shuttle program, due to fuel cell concerns.
STS 83's launch was originally set for 3 April 1997, but was delayed 24 hours on 1 April due to a requirement to add additional thermal insulation to a water coolant line in the orbiter's payload bay. Managers determined that the line, which cools various electronic systems on the orbiter, was not properly insulated and could possibly freeze on-orbit. Liftoff on 4 April 1997 was then delayed an additional 20 minutes, 32 seconds due to an orbiter access hatch seal which had to be replaced.

The first flight of the Microgravity Science Laboratory (MSL-1), the primary payload of STS 83, was cut short due to concerns about one of Columbia's three fuel cells, marking only the third time in the Shuttle program history that a mission ended early. (STS-2, 1981 and STS-44, 1991 were the other two times). Fuel cell number 2 had shown some erratic readings during prelaunch startup, but was cleared to fly after additional checkout and test procedures. Shortly after on-orbit operations began, the number 3 fuel cell substack differential voltage began trending upward. There are three fuel cells on each orbiter, each containing three substacks made up of two banks of 16 cells. In one substack of fuel cell number 2, the difference in output voltage between the two banks of cells was increasing. The fuel cells use a reaction of liquid hydrogen and liquid oxygen to generate electricity and produce drinking water. Although one fuel cell produces enough electricity to conduct on-orbit and landing operations, Shuttle flight rules require all three to be functioning properly to ensure crew safety and provide sufficient backup capability during reentry and landing.

When a purge failed to halt the upward trend, the fuel cell was shut down. Additional purges and other measures failed to correct the anomaly, and around 10 a.m. on 6 April, the Mission Management Team ordered the mission to end early. Fuel cell number 2 was shut down for the remainder of the mission later that afternoon and safed.

The crew was able to conduct some science in the MSL-1 Spacelab module despite the early return. Work was performed in the German electromagnetic levitation furnace facility (TEMPUS) on an experiment called Thermophysical Properties of Undercooled Metallic Melts. This experiment studied the amount of undercooling that can be achieved before solidification occurs. Another experiment performed was the Liquid-Phase Sintering II experiment in the Large Isothermal Furnace. This investigation used heat and pressure to test theories about how the liquefied component bonds with the solid particles of a mixture without reaching the melting point of the new alloy combination.

Also conducted were two fire-related experiments. The Laminar Soot Processes experiment allowed scientists to observe for the first time the concentration and structure of soot from a fire burning in microgravity. The Structure of Flame Balls at Low Lewis-number experiment completed two runs. This experiment was designed to determine under what conditions a stable flame ball can exist, and if heat loss is responsible in some way for the stablilization of the flame ball during burning.

A decision to refly the MSL-1 mission in its entirety was made by the Mission Management Team in the days following Columbia's return. The reflight was first designated STS 83R and then renamed STS 94.

STS 83 ended on 8 April 1997 when Columbia landed on Runway 33, Kennedy Space Center, Florida. Rollout distance: 8,602 feet (2,622 meters). Rollout time: 59 seconds. Mission duration: three days, 23 hours, 12 minutes, 39 seconds. Landed on revolution 64, on the first Kennedy Space Center opportunity for the day.

The flight crew for STS 83 was: James D. Halsell, Mission Commander; Susan L. Still, Pilot; Janice E. Voss, Payload Commander; Donald A. Thomas, Mission Specialist; Michael L. Gernhardt, Mission Specialist; Roger Crouch, Payload Specialist; Greg Linteris, Payload Specialist.

http://www-pao.ksc.nasa.gov/kscpao/chron/sts-83.htm

2002 15:44:19 CDT (GMT -5:00:00)
NASA launched STS 110 (Atlantis 25) carrying the the 43 foot long S0 (S-Zero) Truss to the International Space Station (ISS).
STS 110 lifted off on 8 April 2002 on a mission to install the 43 foot long S0 (S-Zero) Truss, the backbone for future station expansion, to the International Space Station (ISS). While in orbit, the STS-110 crewmembers performed four spacewalks and used the shuttle and station robotic arms to install and outfit the S0. They prepared the station for future spacewalks and spent a week in joint operations with the station's Expedition Four crew. They also prepared the first railroad in space, the Mobile Transporter, for use.

The S0 (S-Zero) Truss is the first of nine pieces that will make up the station's external framework that will eventually span 109 meters (356 feet).

STS 110 Mission Specialist Jerry Ross became the first human to be launched into space seven times. With the two spacewalks that he performed, he tightened his grip on the most US spacewalks (nine) and spacewalking time -- 58 hours, 18 minutes. Second on the list for both spacewalking milestones is Ross' crewmate Mission Specialist Steve Smith, who also conducted two spacewalks during STS 110 to give him a total of 49 hours, 48 minutes during seven spacewalks.

The mission had other spacewalk milestones. This was the first time that the station's robotic arm was used to maneuver spacewalkers around the station, and it was the first time that all of a shuttle crew's spacewalks were based out the station's Quest Airlock.

The flight crew for STS 110 was: Michael J.Bloomfield, Commander; Stephen N. Frick, Pilot; Jerry L. Ross, Mission Specialist; Steven L. Smith, Mission Specialist; Ellen Ochoa, Mission Specialist; Lee M.E. Morin, Mission Specialist; Rex J. Walheim, Mission Specialist.


NASA drawing
http://www.spaceflight.nasa.gov/shuttle/archives/sts-110/index.html

2005
A hybrid solar eclipse will occur, have a path of totality crossing a portion of the Pacific Ocean.
Eclipse map courtesy of Fred Espenak - NASA/Goddard Space Flight Center. For more information on solar and lunar eclipses, see Fred Espenak's Eclipse Home Page:

http://sunearth.gsfc.nasa.gov/eclipse/eclipse.html



2005 Hybrid Eclipse Animation (GIF) by A.T. Sinclair, NASA Goddard Space Flight Center
http://sunearth.gsfc.nasa.gov/eclipse/OH/OH2005.html
http://sunearth.gsfc.nasa.gov/eclipse/SEmono/HSE2005/HSE2005.html


The L5 Development Group membership system is nearing completion for public release. Once it is in place, you will be able to log into your account to modify your newsletter and mailing preferences, etc. Until that time, your only options are to subscribe or unsubscribe from newsletters individually.
Under no circumstances will we release your email address to outside persons or organizations, and it will only be used for mailing the specific information you have requested.

Please help support our efforts by shopping from our sponsors.


Domain registration at http://FKEinternet.com/domains/ - $15.95/year, $29.95 for 2 years

 

This newsletter and its contents are
Copyright © 2006-2010 by The L5 Development Group.  All rights reserved.
 - Publication, in part or in whole, requires previous written permission.
 - Academic or personal-use citations must refer to http://L5Development.com
   as their source.
Thank you for your cooperation.

 

 


Space History Department
Resources
The L5 Development Group Home Page

The L5 Development Group Keyword Access System


Space History for April 8 / Webmaster / Script last modified July 30, 2009 @ 9:27 am
Copyright © 2006-2010 by The L5 Development Group. All rights reserved.

Hosted by FKEinternet