The Hitchhiker Program (HH) was a NASA program established in 1984 and administered by the Goddard Space Flight Center (GSFC) and the Marshall Space Flight Center (MSFC). The program was designed to allow low-cost and quick reactive experiments to be placed on board the Space Shuttle. The program was discontinued after the Space Shuttle Columbia disaster of STS-107.
The National Aeronautics and Space Administration is an independent agency of the United States Federal Government responsible for the civilian space program, as well as aeronautics and aerospace research.
The Goddard Space Flight Center (GSFC) is a major NASA space research laboratory located approximately 6.5 miles (10.5 km) northeast of Washington, D.C. in Greenbelt, Maryland, United States. Established on May 1, 1959 as NASA's first space flight center, GSFC employs approximately 10,000 civil servants and contractors. It is one of ten major NASA field centers, named in recognition of American rocket propulsion pioneer Dr. Robert H. Goddard. GSFC is partially within the former Goddard census-designated place; it has a Greenbelt mailing address.
The George C. Marshall Space Flight Center (MSFC), located in Huntsville, Alabama, is the U.S. government's civilian rocketry and spacecraft propulsion research center. As the largest NASA center, MSFC's first mission was developing the Saturn launch vehicles for the Apollo program. Marshall has been the lead center for the Space Shuttle main propulsion and external tank; payloads and related crew training; International Space Station (ISS) design and assembly; computers, networks, and information management; and the Space Launch System (SLS). Located on the Redstone Arsenal near Huntsville, MSFC is named in honor of Army General George Marshall.
NASA's Hitchhiker project began in early 1984. It was created to accommodate small attached payloads in the Space Shuttle payload bay. Hitchhikers were intended for customers whose space activity requires power, data or command services.
The first Hitchhiker launched on STS-61-C on January 12, 1986. Called HHG-1, it was mounted to the side of the payload bay and carried three experiments. The second Hitchhiker launched on STS-39 on April 28, 1991. This payload was called Space Test Payload (STP)-1 and consisted of five experiments mounted onto a cross-bay carrier. Between 1992 and 1995, 12 Hitchhikers were manifested to fly on the Space Shuttle.
STS-61-C was the 24th mission of NASA's Space Shuttle program, and the seventh mission of Space Shuttle Columbia. It was the first time that Columbia, the first space-rated Space Shuttle orbiter to be constructed, had flown since STS-9. The mission launched from Florida's Kennedy Space Center on 12 January 1986, and landed six days later on 18 January. STS-61-C's seven-person crew included the second African-American shuttle pilot, future NASA Administrator Charles Bolden, the first Costa Rican-born astronaut, Franklin Chang-Diaz, and the second sitting politician to fly in space, Representative Bill Nelson (D-FL). It was the last shuttle mission before the Space Shuttle Challenger disaster, which occurred just ten days after STS-61-C's landing.
STS-39 was the twelfth mission of the Space Shuttle Discovery. The primary purpose of the mission was to conduct a variety of payload experiments for the Department of Defense.
The Hitchhiker system provided real-time communications between the payload and customers in the Hitchhiker control center at Goddard Space Flight Center, Greenbelt, Maryland. The system also provided crew control/display capability, if necessary. Hitchhikers were created to provide a quick reaction and low cost capability for flying small payloads in the Shuttle payload bay.
Greenbelt is a city in Prince George's County, Maryland, United States, and a suburb of Washington, D.C.. Greenbelt is notable for being the first and the largest of the three experimental and controversial New Deal Greenbelt Towns, planned and built by the Federal government of the United States. The cooperative community was conceived in 1935 by Undersecretary of Agriculture Rexford Guy Tugwell, whose perceived collectivist ideology attracted opposition to the Greenbelt Towns project throughout its short duration. The project came into legal existence in the spring of 1935. On April 8, 1935, the United States Congress passed the Emergency Relief Appropriation Act of 1935. Under the authority granted to him from this legislation, President Franklin D. Roosevelt issued an executive order, on May 1, 1935, establishing the United States Resettlement Administration (RA/RRA).
Along with NASA's Get Away Specials (GAS), Hitchhiker was developed and operated by the Goddard Space Flight Center Shuttle Small Payloads Project (SSPP). Unlike Hitchhikers, GAS payloads were only mounted in canisters, did not connect to orbiter electrical services and did not require significant Shuttle support.
Hitchhiker experiments were housed in canisters or attached to mounting plates. The Hitchhiker canister came in two varieties—the Hitchhiker Motorized Door Canister and the Sealed Canisters. The Hitchhiker Motorized Door Canister had mechanical interfaces nearly identical to a GAS canister and could accommodate a customer payload of up to 160 pounds (72.6 kilograms). This canister allowed a payload to be exposed directly to the environment of space.
The Sealed Canister, without a door, could accommodate a customer payload up to 200 pounds (90.7 kilograms). The payload in this canister was sealed in an atmosphere of nitrogen or air.
Nitrogen is the chemical element with the symbol N and atomic number 7. It was first discovered and isolated by Scottish physician Daniel Rutherford in 1772. Although Carl Wilhelm Scheele and Henry Cavendish had independently done so at about the same time, Rutherford is generally accorded the credit because his work was published first. The name nitrogène was suggested by French chemist Jean-Antoine-Claude Chaptal in 1790, when it was found that nitrogen was present in nitric acid and nitrates. Antoine Lavoisier suggested instead the name azote, from the Greek ἀζωτικός "no life", as it is an asphyxiant gas; this name is instead used in many languages, such as French, Russian, Romanian and Turkish, and appears in the English names of some nitrogen compounds such as hydrazine, azides and azo compounds.
Experiments attached to mounting plates could be placed on the vertical plate, a 25 inches (63.5 centimeters) by 39 inches (99.1 centimeters) mounting surface for up to 200 pounds (90.7 kilograms) of customer hardware. A larger mounting plate measured 50 inches (127 centimeters) by 60 inches (152.4 centimeters). This plate, available for use on the side-mount carrier, was for larger experiments or hardware requirements. Customer hardware mounted on plates may have needed additional customer-provided thermal control provisions, such as heaters or blankets.
Launch Date | STS Number | Payload Name | Payload Classification | Experiment Name | Payload Carrier Hardware |
---|---|---|---|---|---|
03/22/82 | 3 | GAS, FVP | GAS | GAS, FVP | Adapter Beam |
06/27/82 | 4 | G-001 | GAS | G-001 | Adapter Beam |
11/11/82 | 5 | G-026 | GAS | G-026 | Adapter Beam |
04/04/83 | 6 | G-005 G-049 G-381 | GAS | G-005 G-049 G-381 | Adapter Beam |
06/18/83 | 7 | G-002 G-088 G-009 G-012 G-033 G-305 G-345 | GAS | G-002 G-088 G-009 G-012 G-033 G-305 G-345 | Adapter Beam |
08/30/83 | 8 | G-346 G-347 | GAS | G-346 G-347 | Adapter Beam |
02/03/84 | 10 (41-B) | G-004 G-008 | GAS | G-004 G-008 | Adapter Beam |
10/05/84 | 13 (41-G) | G-007 G-013 | GAS | G-007 G-013 | Adapter Beam |
04/12/85 | 16 (51-D) | G-035 G-471 | GAS | G-035 G-471 | Adapter Beam |
04/29//85 | 17 (51-B) | G-010 G-308 | GAS | G-010 G-308 | Adapter Beam |
06/17/85 | 18 (51-G) | G-025 G-027 | GAS | G-025 G-027 | Adapter Beam |
10/30/85 | 22 (61-A) | G-308 | GAS | G-308 | Adapter Beam |
11/26/85 | 23 (61-B) | G-479 | GAS | G-479 | Adapter Beam |
01/12/86 | 24 (61-C) | HHG-1 | Hitchhiker | Particle Analysis Cameras for the Capillary Pump | Hitchhiker Bridge |
01/12/86 | 24 (61-C) | GBA-1 | GAS Bridge Assembly-1 | G-007 G-062 | GAS Assembly Bridge (GBA) |
08/08/89 | 28 | G-335 G-341 | GAS | G-335 G-341 | Adapter Beam |
10/18/89 | 34 | Shuttle Solar Background Ultraviolet (SSBUV-01) | Adapter Beam | Shuttle Solar Background Ultraviolet | Adapter Beam |
12/02/90 | 35 | Broad Band X-Ray Telescope (BBXRT) | HH | Broad Band X-Ray Telescope
| Adapter Beam |
04/28/91 | 39 | <acronym title="Multi- Purpose Experiment Canister">MPEC</acronym>-01 | CAP | Multi- Purpose Experiment Canister (MPEC) | Adapter Beam |
04/28/91 | 39 | <acronym title="Space Test Payload">Space Test Payload (STP)-1</acronym> | HH | Advanced Liquid Data Systems Experiment (DSE), <acronym title="National Aeronautics and Space Administration">NASA</acronym><acronym title="Goddard Space Flight Center">GSFC</acronym> Spacecraft Kinetic Infrared Test Ultraviolet Limb Imaging Experiment (UVLIMB), <acronym title="Naval Research Laboratory"> | Hitchhiker Bridge |
06/05/91 | 40 | GBA-2 | GAS | G-021 G-052 | GBA |
01/22/92 | 42 | GBA-3 | GAS Bridge Assembly-3 | G-086 G-140 | GBA |
08/02/91 | 43 | TPCE-01 | CAP | TPCE-01 | Adapter Beam |
03/24/92 | 45 | G-229 | GAS | G-229 | Adapter Beam |
07/31/92 | 46 | <acronym title="Consortium Complex Autonomous Payload">CONCAP IV-03</acronym>-II-01 | CAP | <acronym title="Limited Duration Space Environment Candidate Materials Exposure">LDCE</acronym>-01 LDCE-02 | Adapter Beam |
09/12/92 | 47 | GBA-4 | GAS | G-102 G-255 | Adapter Beam |
11/12/93 | 51 | LDCE-04 LDCE-05 | CAP | LDCE-04 LDCE-05 | Adapter Beam |
10/22/92 | 52 | <acronym title="Attitude Sensor Package">ASP</acronym> | HH | Attitude Sensor Package (ASP) | Adapter Beam |
10/22/92 | 52 | TPCE-01 | CAP | TPCE-01 | Adapter Beam |
12/02/92 | 53 | GCP | HH | Orbital Debris Cryogenic Shuttle Glow | Adapter Beam |
01/13/93 | 54 | <acronym title="Diffuse X-ray Spectrometer">DXS</acronym> | HH | Diffuse X-ray Spectrometer (DXS) | Adapter Beam |
04/26/93 | 55 | <acronym title="Reaction Kinetics in Glass Melts">RKGM</acronym> | CAP | RKGM | Adapter Beam |
04/08/93 | 56 | <acronym title="Solar Ultra-Violet Experiment">SUVE</acronym> | CAP | SUVE | Adapter Beam |
06/21/93 | 57 | <acronym title="Super Fluid Helium On Orbit Transfer">SHOOT</acronym> | HH | Super Fluid Helium On Orbit Transfer (SHOOT) | Adapter Beam |
06/21/93 | 57 | GBA-5 | GAS | CONCAP-IV-01 G-022 | GBA |
04/09/94 | 59 | CONCAP IV-02 <acronym title="Goddard ground support equipment"></acronym> | CAP | CONCAP IV-02 | Adapter Beam |
04/09/94 | 59 | G-203 G-300 | GAS | G-203 G-300 | Adapter Beam |
02/03/94 | 60 | COB/GBA ODERACS-1R | GAS Bridge Assembly-6 with Hitchhiker Avionic | Capillary Pumped Loop (CAPL), | GBA w/ HH Avionics |
02/03/94 | 60 | COB/GBA ODERACS-1R BREMSAT | HH | Orbital Debris Radar Calibration Spheres (ODERACS-1R), | GBA w/ HH Avionics |
02/03/94 | 6 0 | COB/GBA ODERACS-1R BREMSAT | CAP | BREMAN Satellite (BREMSAT), University of Bremen | GBA w/ HH Avionics |
02/03/94 | 60 | COB/GBA ODERACS-1R BREMSAT | GAS | G-071 | GBA w/ HH Avionics |
03/04/94 | 62 | LDCE-06 LDCE-07 LDCE-08 | CAP | LDCE-06 LDCE-07 LDCE-08 | Adapter Beam |
03/04/94 | 62 | <acronym title="Office of Aeronautics and Space Technology">OAST</acronym>-2 | CAP | Thermal Energy Storage (TES-1, | HH Bridge |
03/04/94 | 62 | <acronym title="Office of Aeronautics and Space Technology">OAST</acronym>-2 | HH | Cryogenic Two Phase (CRYOTP), NASA GSFC/USAF Phillips Lab Emulsion Chamber Technology (ECT), NASA MSFC Experimental Investigation of Spacecraft Glow (EISG), NASA JSC/NASA GSFC Solar Array Module Plasma Interaction Experiment Spacecraft Kinetic Infrared Test | HH Bridge |
02/03/95 | 63 | CGP/<acronym title="orbital debris radar calibration sphere">ODERACS</acronym>-2 | HH | Cryo System Experiment (CSE), Hughes Shuttle Glow IMAX Cargo Bay Camera (ICBC) Orbital Debris | HH Bridge |
09/09/94 | 64 | <acronym title="Robot Operated Materials Processing System">ROMPS</acronym>-1 | HH | Robot Operated Materials Processing System (ROMPS) | Adapter Beam |
09/09/94 | 64 | GBA-7 | GAS | G-178 G-254 | GBA |
11/03/94 | 66 | ESCAPE-2 | CAP | ESCAPE-2 | Adapter Beam |
03/02/95 | 67 | G-387 G-388 | GAS | G-387 G-388 | Adapter Beam |
09/30/94 | 68 | G-316 | GAS | G-316 G-503 G-541 | Adapter Beam |
09/07/95 | 69 | <acronym title="International EUV Hitchhiker">IEH-1</acronym> | HH | Ultraviolet Spectrograph Telescope for Astronomical Shuttle Glow Experiment-3 Solar Extreme Ultraviolet HH | HH Bridge |
09/07/95 | 69 | IEH-1 | HH-Jr. | Complex Autonomous | HH Bridge |
09/07/95 | 69 | <acronym title="Capillary Pumped Loop/Get Away Special Bridge Assembly">CAPL/GBA</acronym> | HH | Capillary Pumped Loop (CAPL-2), NASA/GSFC | GBA |
09/07/95 | 69 | CAPL/GBA | CAP | TES-2 | GBA |
09/07/95 | 69 | CAPL/GBA | GAS | G-515 | GBA |
01/11/96 | 72 | SLA-01 | HH | Shuttle Laser Altimeter-01 (SLA-01), NASA/GSFC | HH Bridge |
01/11/96 | 72 | SLA-01 | CAP | TES-2 | HH Bridge |
01/11/96 | 72 | SLA-01 | GAS | G-342 | HH Bridge |
01/11/96 | 72 | SLA-01 | HH | Shuttle Laser Altimeter-01(SLA-01), NASA/GSFC | HH Bridge |
11/12/95 | 74 | GPP | HH | Shuttle Glow Experiment (GLO-4) Photogrammetric Appendage Structural Dynamics Experiment Payload (PASDE-01) | Adapter Beam |
03/22/96 | 76 | G-312 | GAS | G-312 | Adapter Beam |
05/19/96 | 77 | TEAMS | HH | Vented Tank Resupply Experiment (VTRE), NASA/LeRC GPS Attitude and Navigation Experiment (GANE), NASA/JSC Liquid Metal Thermal Experiment (LMTE), USAF Phillips Laboratory Passive Aerodynamically-Stabilized Magnetically-Damped Satellite (PAMS), NASA GSFC | HH Bridge |
05/19/96 | 77 | TPCE-RF | CAP | TPCE-RF | GBA |
05/19/96 | 77 | G-056 G-063 G-142 G-144 G-163 G-200 G-490 G-564 G-565 G-703 G-741 | GAS | G-056 G-063 G-142 G-144 G-163 G-200 G-490 G-564 G-565 G-703 G-741 | GBA |
11/19/96 | 80 | SEM-01 | SEM | SEM-01 | Adapter Beam |
04/04/97 | 83 | CRYOFD | HH | Cryogenic Flexible Diode (CRYOFD), NASA GSFC/USAF Phillips Lab | Adapter Beam |
08/07/97 | 85 | TAS-01 | HH | Shuttle Laser Altimeter (SLA-02), NASA GSFC Infrared Spectral Imaging Radiometer (ISIR), NASA GSFC Critical Viscosity of Xenon (CVX-01), NASA LeRC Space Experiment Module (SEM-02), NASA GSFC Solar Constant (SOLCON-1), Royal Meteorological Institute of Belgium Two-Phase Flow (TPF), NASA GSFC COOLLAR Flight Experiment (CFE), USAF Phillips Lab | HH Bridge |
08/07/97 | 85 | TAS-01 | SEM | SEM-02 | HH Bridge |
08/07/97 | 85 | IEH-2 | HH | Ultraviolet Spectrograph Telescope for Astronomical Research (UVSTAR), U of AZ/ESA Shuttle Glow Experiment-5 & 6 (GLO-5 & 6), U of AZ Solar Extreme Ultraviolet Hitchhiker (SEH), USC Distribution and Automation Technology Advancement - Colorado Hitchhiker And Student Experiment of solar Radiation (DATA-CHASER), University of Colorado | HH Bridge |
08/07/97 | 85 | G-572 G-745 | GAS | G-572 G-745 | Adapter Beam |
19/25/97 | 86 | SEEDSII | CAP | SEEDSII | Adapter Beam |
11/19/97 | 87 | LHP/NaSBE (LNBP) | HH | Loop Heat Pipe Experiment (LHP), Dynatherm Sodium Surface Battery Experiment (NaSBE), NRL | Adapter Beam |
11/19/97 | 87 | SOLSE-01 | HH-Jr | Shuttle Ozone Limb Sounding Experiment (SOLSE-01), NASA GSFC | Adapter Beam |
11/19/97 | 87 | TGDF | CAP | TGDF | Adapter Beam |
11/19/97 | 87 | G-036 | GAS | G-036 | Adapter Beam |
12/04/98 | 88 | MIGHTYSAT-1 | HH | MightySat-1, USAF Phillips Lab | Adapter Beam |
12/04/98 | 88 | JSC APFR | HH | JSC APFR | Adapter Beam |
12/04/98 | 88 | G-093R | GAS | G-093R | Adapter Beam |
12/04/98 | 88 | SEM-07 | SEM | SEM-07 | Adapter Beam |
01/22/98 | 89 | G-093 | GAS | G-093 G-141 G-145 G-432 | Adapter Beam |
04/17/98 | 90 | SVF-01 | CAP | Shuttle Vibration Forces (SVF), NASA JPL | Adapter Beam |
04/17/98 | 90 | G-197 G-744 G-772 | GAS | G-197 G-744 G-772 | Adapter Beam |
06/02/98 | 91 | G-090 | GAS | G-090 G-648 G-743 G-765 | Adapter Beam |
06/02/98 | 91 | SEM-03 | SEM | SEM-03 SEM-05 | Adapter Beam |
07/01/97 | 94 | CRYOFD | HH | Cryogenic Flexible Diode (CRYOFD) experiment payload | Adapter Beam |
10/29/98 | 95 | CRYOTSU | HH | Cryogenic Thermal Storage Unit (CRYOTSU), NASA GSFC | Adapter Beam |
10/29/98 | 95 | IEH-3 | HH | Ultraviolet Spectrograph Telescope for Astronomical Research (UVSTAR), U of AZ/ESA Solar Extreme Ultraviolet Hitchhiker (SEH), USC STAR-LITE, U of AZ Petite Amateur Navy Satellite (PANSAT), USAF Space Test Program Solar Constant Experiment (SOLCON-02), Royal Meteorological Institute of Belgium | HH Bridge |
10/29/98 | 95 | IEH-3 | GAS | G-238 | HH Bridge |
10/29/98 | 95 | SEM-04 | SEM | SEM-04 | SEM-attached to SPARTAN 201-05 Bridge |
10/29/98 | 95 | G-467 G-779 | GAS | G-467 G-779 | Adapter Beam |
05/27/99 | 96 | SVF-02 | CAP | Shuttle Vibration Forces (SVF-02), NASA JPL | Adapter Beam |
05/27/99 | 96 | STARSHINE | HH | Student Tracked Atmospheric Research Satellite for Heuristic International Networking Experiment (STARSHINE), Rocky Mountain NASA Space Grant Consortium/USU | Adapter Beam |
05/19/00 | 101 | MARS | CAP | MARS | Adapter Beam |
05/19/00 | 101 | SEM-06 | SEM | SEM-06 | Adapter Beam |
03/08/01 | 102 | WSVFM | CAP | Wide-band Shuttle Vibration Force Measurement(WSVFM) NASA JPL | Adapter Beam |
03/08/01 | 102 | G-783 | GAS | G-783 | Adapter Beam |
03/08/01 | 102 | SEM-09 | SEM | SEM-09 | Adapter Beam |
03/08/01 | 102 | Beam - Bay 4 | Beam - Contingency I | Beam - Bay 4 | Adapter Beam |
08/10/01 | 105 | HEAT | HH | Advance Carrier Equipment (ACE) SimpleSat, NASA/GSFC | Adapter Beam |
08/10/01 | 105 | HEAT | GAS | G-774 | |
08/10/01 | 105 | HEAT | SEM | SEM-10 | Adapter Beam |
08/10/01 | 105 | G-780 | GAS | G-780 | Adapter Beam |
08/10/01 | 105 | HEAT | Beam - Bay 4 Port | Beam for Contingency | Adapter Beam |
09/08/00 | 106 | G-782 | GAS | G-782 | Adapter Beam |
09/08/00 | 106 | SEM-08 | SEM | SEM-08 | Adapter Beam |
11/29/02 | 107 | FREESTAR | HH | Mediterranean Israeli Dust Experiment (MEIDEX), Israeli Space Agency Solar Constant Experiment (SOLCON-03), Royal Meteorological Institute of Belgium Shuttle Ozone Limb Sounding Experiment (SOLSE-2), NASA GSFC Critical Viscosity of Xenon (CVX-2), NASA GRC Low Power Transceiver (LPT), NASA GSFC and ITT Industries
| HH Bridge |
11/29/02 | 107 | FREESTAR | HH | SEM-14 | HH Bridge |
12/05/01 | 108 | MACH-1 | HH | CAPL-3, NASA GSFC and the Naval Research Laboratory STARSHINE-2, Rocky Mountain NASA Space Grant Consortium / USU Prototype Synchrotron Radiation Detector (PSRD), NASA JSC | GBA with HH Avionics |
12/05/01 | 108 | MACH-1 | CAP | Collisions Into Dust Experiment (COLLIDE-2), NASA GRC | GBA with HH Avionics |
12/05/01 | 108 | MACH-1 | GAS | G-761 | GBA with HH Avionics |
12/05/01 | 108 | MACH-1 | SEM | SEM-11 | GBA with HH Avionics |
12/05/01 | 108 | LMC | LMC Carrier | SEM-12 | LMC Carrier |
12/05/01 | 108 | LMC | LMC Carrier | G-064 | LMC Carrier |
12/05/01 | 108 | G-221 G-775 | GAS | G-221 | Adapter Beam</tbody> |
The Hitchhiker carrier system was modular and expandable in accordance with payload requirements. This flexibility allowed maximum efficiency in utilizing orbiter resources and increased the potential for early manifesting on the shuttle.
There were two types of carrier systems—the Hitchhiker Side-Mount Carrier System and the Hitchhiker Cross-Bay Bridge Carrier System. Either system could accept the Hitchhiker canister and the mounting plates.
The Hitchhiker Side-Mount Carrier System used a GAS Adapter Beam for all equipment. The beam attached to the orbiter frame. The side-mount carrier was usually installed in the forward starboard side of the payload bay, although other configurations and locations were possible. This carrier could hold up to three experiments and the Hitchhiker avionics box, which connected the power, data and signal from the shuttle to the experiments.
The Hitchhiker Cross-Bay Carrier could be located anywhere in the payload bay. The carrier could accommodate 11 Hitchhiker canisters or 11 of the smaller mounting plates. There was also room for the necessary avionic units.
Four additional mounting slots were located on the top of the carrier and could accept 33 inch (83.8 centimeter) by 27 inch (68.6 centimeter) pallets or 33 inch (83.8 centimeter) by 55 inch (139.7 centimeter) pallets in any combination with up to 500 pounds (226.8 kilograms) of equipment. Any customer experiments and hardware that could be mounted on the side-mount carrier could also be flown on the cross-bay carrier.
NASA created Hitchhikers to provide customers with a way to send small payloads into orbit on the Space Shuttle. This was done with a short turn-around-time—from manifest to flight took an average of 18 months. To keep the project on schedule, experiments needed to fit in canisters or on mounting plates and meet standard mechanical and electrical interfaces.
Because the payload met these conditions, it also was entitled to special "handling" in the orbiter that other small payloads, like the Get Away Specials did not receive. This special handling included tapping into the Shuttle for power and "astronaut" services," such as requiring specific shuttle attitudes or maneuvers. The orbiter crew moved the Shuttle when necessary to the position needed for the Hitchhiker experiment, provided it did not interfere with the needs of the primary payloads.
Hitchhikers were manifested to fly with primary payloads that either have similar requirements or that will not be affected by the changes in shuttle position necessary to the Hitchhiker experiments. In addition to making adjustments to the orbiter, the astronaut crew participated in the Hitchhiker experiments by controlling the flow of orbiter power on or off using two switches located on the Standard Switch Panel.
The first switch controlled power to the avionics unit. The second switch allowed power to flow from the avionics unit to the experiment. This simple measure allowed the astronauts to have some control over the experiment, in the event of a problem. For some payloads, the crew had a keyboard/display unit, for additional control.
Getting the power from the shuttle to the payload required an avionics unit. This unit connected the power from the shuttle to the experiment. The avionics unit also carried the equipment for transmitting the data real-time to the ground control center. The avionics unit also contained the relay switching equipment and had the connections for the customer to use the shuttle television system, and the crew control/display system. Each avionics unit could handle the requirements for six experiments.
Goddard was responsible for the management and operation of the Hitchhiker project through the Shuttle Small Payloads Project. In this capacity Goddard provided the Hitchhiker carriers and the avionics unit.
During the mission, customers used a control center located at Goddard. The customer provided Ground System Equipment (CGSE), software and personnel to generate commands to the payload and display data from the payload during flight, as well as during payload-to-carrier integration and verification testing.
The Hitchhiker carrier system was equipped with a "transparent" data system which allowed customers to easily use their existing ground equipment and software to control their experiments during flight. Data was sent down to the control center in real time, but it also was recorded at Goddard once it reached the ground. The data was transmitted over Goddard's Tracking and Data Relay Satellite System.
The Space Shuttle was a partially reusable low Earth orbital spacecraft system that was operated from 1981 to 2011 by the U.S. National Aeronautics and Space Administration (NASA) as part of the Space Shuttle program. Its official program name was Space Transportation System (STS), taken from a 1969 plan for a system of reusable spacecraft of which it was the only item funded for development. The first of four orbital test flights occurred in 1981, leading to operational flights beginning in 1982. In addition to the prototype whose completion was cancelled, five complete Shuttle systems were built and used on a total of 135 missions from 1981 to 2011, launched from the Kennedy Space Center (KSC) in Florida. Operational missions launched numerous satellites, interplanetary probes, and the Hubble Space Telescope (HST); conducted science experiments in orbit; and participated in construction and servicing of the International Space Station. The Shuttle fleet's total mission time was 1322 days, 19 hours, 21 minutes and 23 seconds.
Spacelab was a reusable laboratory developed by ESA and used on certain spaceflights flown by the Space Shuttle. The laboratory comprised multiple components, including a pressurized module, an unpressurized carrier and other related hardware housed in the Shuttle's cargo bay. The components were arranged in various configurations to meet the needs of each spaceflight.
STS-35 was the tenth flight of Space Shuttle Columbia, the 38th shuttle flight, and a mission devoted to astronomical observations with ASTRO-1, a Spacelab observatory consisting of four telescopes. The mission launched from Kennedy Space Center in Florida on 2 December 1990.
STS-52 was a Space Transportation System mission using Space Shuttle Columbia, and was launched on 22 October 1992.
STS-54 was a Space Transportation System mission using Space Shuttle Endeavour. This was the third flight for Endeavour, and was launched on 13 January 1993.
STS-51 was a Space Shuttle Discovery mission that launched the Advanced Communications Technology Satellite (ACTS) in September 1993. The flight also featured the deployment and retrieval of the SPAS-ORFEUS satellite and its IMAX camera, which captured spectacular footage of Discovery in space. A spacewalk was also performed during the mission to evaluate tools and techniques for the STS-61 Hubble Space Telescope servicing mission later that year. STS-51 was the first shuttle mission to fly a GPS receiver, a Trimble TANS Quadrex. It was mounted in an overhead window where limited field of view and signal attenuation from the glass severely impacted receiver performance.
STS-63 was the first mission of the US/Russian Shuttle-Mir Program, which carried out the first rendezvous of the American Space Shuttle with Russia's space station Mir. Known as the 'Near-Mir' mission, the flight used Space Shuttle Discovery, which lifted off from launch pad 39B on 3 February 1995 from Kennedy Space Center, Florida. A night launch and the 20th mission for Discovery, it marked the first time a Space Shuttle mission had a female pilot, Eileen Collins, the first EVAs for both a UK born astronaut Michael Foale and a US astronaut of African heritage Bernard A. Harris, Jr. and it also carried out the successful deployment and retrieval of the Spartan-204 platform, along with the scheduled rendezvous and flyaround of Mir, in preparation for STS-71, the first mission to dock with Mir.
STS-69 was a Space Shuttle Endeavour mission, and the second flight of the Wake Shield Facility (WSF). The mission launched from Kennedy Space Center, Florida on 7 September 1995. It was the 100th successful manned NASA spaceflight, not including X-15 flights.
STS-74 was the fourth mission of the US/Russian Shuttle-Mir Program, and the second docking of the Space Shuttle with Mir. Space Shuttle Atlantis lifted off from Kennedy Space Center launch pad 39A on 12 November 1995. The mission ended 8 days later with the landing of Atlantis back at Kennedy. It was the second in a series of seven straight missions to the station flown by Atlantis.
STS-72 was a Space Shuttle Endeavour mission to capture and return to Earth a Japanese microgravity research spacecraft known as Space Flyer Unit (SFU). The mission launched from Kennedy Space Center, Florida on 11 January 1996.
STS-87 was a Space Shuttle mission launched from Launch Complex 39B of the Kennedy Space Center on 19 November 1997. It was the 88th flight of the Space Shuttle, and the 24th flight of Columbia. The mission goals were to conduct experiments using the United States Microgravity Payload (USMP-4), conduct two EVAs, and to deploy the SPARTAN-201 experiment. This mission marked the first time an EVA was performed from Columbia. An EVA from Columbia was originally planned for STS-5 in 1982, but was cancelled due to spacesuit problems. It also marked the first EVA conducted by a Japanese astronaut, Takao Doi.
STS-95 was a Space Shuttle mission launched from Kennedy Space Center, Florida on 29 October 1998, using the orbiter Discovery. It was the 25th flight of Discovery and the 92nd mission flown since the start of the Space Shuttle program in April 1981. It was a highly publicized mission due to former Project Mercury astronaut and United States Senator John H. Glenn, Jr.'s return to space for his second space flight. At age 77, Glenn became the oldest person, to date, to go into space. This mission is also noted for inaugurating ATSC HDTV broadcasting in the U.S., with live coast-to-coast coverage of the launch. In another first, Pedro Duque became the first Spaniard in space.
STS-96 was a Space Shuttle mission to the International Space Station (ISS) flown by Space Shuttle Discovery, and the first shuttle flight to dock with the International Space Station. The shuttle carried the Spacehab module in the payload, filled with cargo for station outfitting. STS-96 launched from Kennedy Space Center, Florida, on 27 May 1999 at 06:49:42 AM EDT.
STS-105 was a mission of the Space Shuttle Discovery to the International Space Station, launched from Kennedy Space Center, Florida, 10 August 2001. This mission was Discovery's final mission until STS-114, because Discovery was grounded for a refit, and then all Shuttles were grounded in the wake of the Columbia disaster. The refit included an update of the flight deck to the glass cockpit layout, which was already installed on Atlantis and Columbia.
STS-108 was a Space Shuttle mission to the International Space Station (ISS) flown by Space Shuttle Endeavour. Its primary objective was to deliver supplies to and help maintain the ISS.
Getaway Special was a NASA program that offered interested individuals, or groups, opportunities to fly small experiments aboard the Space Shuttle. Over the 20-year history of the program, over 170 individual missions were flown. The program, which was officially known as the Small, Self-Contained Payloads program, was canceled following the Space Shuttle Columbia disaster on February 1, 2003.
An ExPRESS logistics carrier (ELC) is an unpressurized attached payload platform for the International Space Station (ISS) that provides mechanical mounting surfaces, electrical power, and command and data handling services for Orbital Replacement Units (ORUs) as well as science experiments on the ISS. The ELCs were developed primarily at the Goddard Space Flight Center in Greenbelt, Maryland, with support from JSC, KSC, and MSFC. ELC was formerly called "Express Pallet" and is the unpressurized counterpart to the pressurized ExPRESS Rack. An ELC provides scientists with a platform and infrastructure to deploy experiments in the vacuum of space without requiring a separate dedicated Earth-orbiting satellite.
FREESTAR, which stands for Fast Reaction Experiments Enabling Science TechnologyApplications and Research, was a payload of six separate experiments on the Space Shuttle Columbia.
Integrated Cargo Carrier (ICC) was a project, started in 1997 by the companies Spacehab and Airbus DS Space Systems, to develop a family of flight proven and certified cross-the-bay cargo carriers designed to fly inside the Space Shuttle cargo bay, installed either horizontally or vertically, and able to carry up to 8000 lbs. of unpressurized cargo into orbit. Airbus owns the ICC fleet of carriers.