OV2-3

Last updated
OV2-3
OV2SP133.jpg
An OV-2 satellite
Mission type Life science
Operator USAF
COSPAR ID 1965-108A
SATCAT no. 13912 OOjs UI icon edit-ltr-progressive.svg
Spacecraft properties
Manufacturer Northrop
Launch mass194 kg (428 lb)
Start of mission
Launch date22 December 1965, 14:00:01 (1965-12-22UTC14:00:01) UTC
Rocket Titan IIIC
Launch site Cape Canaveral LC41 [1]
Orbital parameters
Reference system Geocentric
Regime Highly elliptical
Eccentricity 0.71885
Perigee altitude 167 km (104 mi)
Apogee altitude 33,662 km (20,917 mi)
Inclination 26.300°
Period 589.20 minutes [2]
Epoch 21 December 1965
  OV2-1
OV2-5  
 

Orbiting Vehicle 2-3 (COSPAR ID: 1965-108A, also known as OV2-3), the second satellite of the second series of the United States Air Force's Orbiting Vehicle program, was an American solar astronomy, geomagnetic and particle science research satellite. Launched 22 December 1965 along with three other satellites, the mission resulted in failure when the spacecraft failed to separate from the upper stage of its Titan IIIC. [2]

Contents

Background

The Orbiting Vehicle satellite program arose from a US Air Force initiative, begun in the early 1960s, to reduce the expense of space research. Through this initiative, satellites would be standardized to improve reliability and cost-efficiency, and where possible, they would fly on test vehicles or be piggybacked with other satellites. In 1961, the Air Force Office of Aerospace Research (OAR) created the Aerospace Research Support Program (ARSP) to request satellite research proposals and choose mission experiments. The USAF Space and Missiles Organization created their own analog of the ARSP called the Space Experiments Support Program (SESP), which sponsored a greater proportion of technological experiments than the ARSP. [3] :417 Five distinct OV series of standardized satellites were developed under the auspices of these agencies. [3] :425

The OV2 series of satellites was originally designed as part of the ARENTS (Advanced Research Environmental Test Satellite) program, intended to obtain supporting data for the Vela satellites, which monitored the Earth for violations of the 1963 Partial Test Ban Treaty. Upon the cancellation of ARENTS due to delays in the Centaur rocket stage, the program's hardware (developed by General Dynamics) was repurposed to fly on the Titan III [3] :422 (initially the A, [4] ultimately the C) booster test launches. [3] :422 The USAF contracted Northrop to produce these satellites, with William C. Armstrong of Northrop Space Laboratories serving as the program manager. [4]

The first satellite in the OV2 series, OV2-1, was launched 15 October 1965 with a suite of radiation measuring experiments; it was lost when its booster broke up in orbit. [5] The next satellite in the series, OV2-2, was to carry out optical measurements from an altitude of 400 kilometres (250 mi), but the mission was cancelled when the Titan III test schedule was truncated. Instead, OV2-3, with several solar experiments, was scheduled for the next Titan III launch. [3] :422

Spacecraft design

OV2-3 was built to the configuration standard to all of the OV2 satellites, with a roughly cubical structure of aluminum honeycomb, .61 m (2.0 ft) in height, and .58 m (1.9 ft) wide. Four 2.3 m (7.5 ft) paddle-like solar panels, each with 20,160 solar cells, were mounted at the four upper corners of the main body. The power system, which included NiCd batteries for night-time operations, provided 63 W of power. As with the other craft in the OV2 series, experiments were generally mounted outside the cube while satellite systems, including tape recorder, command receiver, and PAM/FM/FM telemetry system, were installed inside. Four small solid rocket motors spun, one on each paddle, were designed to spin the OV2 satellites upon reaching orbit, providing gyroscopic stability. Cold-gas jets maintained this stability, receiving information on the satellite's alignment with respect to the Sun via an onboard solar aspect sensor, and with respect to the local magnetic field via two onboard fluxgate magnetometers. A damper kept the satellite from precessing (wobbling around its spin axis). Passive thermal control kept the satellite from overheating. [3] :422 The entire satellite weighed 194 kg (428 lb). [6]

Experiments

The Air Force's Cambridge Research Center in conjunction with Space Systems Division and Aerospace Corporation [4] designed the scientific and engineering experiment package of fifteen instruments designed to measure radiation of solar and geomagnetic origin. [6]

Mission

Titan 3C launch 22 Dec 1965 Titan3C launch 22 Dec 1965.jpg
Titan 3C launch 22 Dec 1965

OV2-3, along with LES-3, LES-4, and OSCAR 4, was launched on the third Titan IIIC test flight [6] on 22 December 1965 at 14:00:01 UT from Cape Canaveral LC41 [1] just one second behind schedule. From an initial parking orbit of 194 kilometres (121 mi), the Titan's Transtage boosted into a transfer orbit pending a final burn to circularize its orbit. However, this final burn, scheduled for T+6:03:04 after liftoff, [6] never occurred due to a leaking valve in the booster's attitude control system. [3] :422 LES-3, LES-4, and OSCAR 4 were released from the Transtage, albeit much later than intended, [6] but OV2-3 remained attached and did not operate. [3] :422

Legacy and status

The satellite and its Transtage are still in orbit as of November 2020. [7]

The OV2 series continued with the radiation and astronomical satellite, OV2-5, which achieved a degree of success. [8]

Related Research Articles

Titan (rocket family) Family of expendable launch vehicles used in U.S. Air Force and space programs (1959-2005)

Titan was a family of United States expendable rockets used between 1959 and 2005. The Titan I and Titan II were part of the US Air Force's intercontinental ballistic missile fleet until 1987. The space launch vehicle versions contributed the majority of the 368 Titan launches, including all the Project Gemini crewed flights of the mid-1960s. Titan vehicles were also used to lift US military payloads as well as civilian agency reconnaissance satellites and to send interplanetary scientific probes throughout the Solar System.

Titan IIIC

The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. It was the first Titan booster to feature large solid rocket motors and was planned to be used as a launcher for the Dyna-Soar, though the spaceplane was cancelled before it could fly. The majority of the launcher's payloads were DoD satellites, for military communications and early warning, though one flight (ATS-6) was performed by NASA. The Titan IIIC was launched exclusively from Cape Canaveral while its sibling, the Titan IIID, was launched only from Vandenberg AFB.

Titan IIIA

The Titan IIIA or Titan 3A was an American expendable launch system, launched four times in 1964 and 1965, to test the Transtage upper stage which was intended for use on the larger Titan IIIC. The Transtage was mounted atop two core stages derived from the Titan II. The Titan IIIA was also used as the core of the Titan IIIC.

Orbiting Vehicle or OV, originally designated SATAR, comprised five disparate series of standardized American satellites operated by the US Air Force, launched between 1965 and 1971. Forty seven satellites were built, of which forty three were launched and thirty seven reached orbit. With the exception of the OV3 series and OV4-3, they were launched as secondary payloads, using excess space on other missions.

OPS 0855 American boilerplate Manned Orbital Laboratory spacecraft

OPS 0855, also designated OV4-3, was an American boilerplate Manned Orbiting Laboratory spacecraft launched in 1966. It was flown to demonstrate the launch configuration for future MOL missions. A number of research payloads, designated Manifold, were carried on board, which were intended to operate for 75 days. However, the spacecraft ceased operations after just 30. It was built from a decommissioned HGM-25A Titan I first stage oxidizer tank, bolted to a Transtage. It was part of the MOL and Orbiting Vehicle projects.

6555th Aerospace Test Group

The 6555th Aerospace Test Group is an inactive United States Air Force unit. It was last assigned to the Eastern Space and Missile Center and stationed at Patrick Air Force Base, Florida. It was inactivated on 1 October 1990.

Artemis 1 Planned test flight of Orion spacecraft and initial flight of the Space Launch System for Artemis program

Artemis 1 is a planned uncrewed test flight for NASA's Artemis program that is the first integrated flight of the agency's Orion MPCV and Space Launch System heavy-lift rocket. It is expected to launch on 4 November 2021.

OSCAR 4

OSCAR IV was the fourth amateur radio satellite launched by Project OSCAR and the first targeted for Geostationary orbit on 12 December 1965. The satellite was launched piggyback with three United States Air Force satellites on a Titan IIIC launch vehicle. Due to a booster failure, OSCAR 4 was placed in an unplanned and largely unusable Geostationary transfer orbit; however, OSCAR 4 did facilitate the first direct satellite communication between the United States and the USSR.

OV2-1 US Air Force satellite

Orbiting Vehicle 2-1, the first satellite of the second series of the United States Air Force's Orbiting Vehicle program, was an American life science research satellite. Its purpose was to determine the extent of the threat posed to astronauts by the Van Allen radiation belts. Launched 15 October 1965, the mission resulted in failure when the upper stage of OV2-1's Titan IIIC booster broke up.

OV1-1 US Air Force satellite

Orbiting Vehicle 1-1, was the first satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-1 was an American Earth science research satellite designed to measure radiation, micrometeoroid density, and magnetic fields in orbit. Launched 21 January 1965, the mission resulted in failure when, after a successful launch of its Atlas booster, OV1-1's onboard Altair motor failed to fire.

OV1-3 US Air Force satellite

Orbiting Vehicle 1-3, was the second satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-3 was an American life science research satellite designed to measure the effects of orbital radiation on the human body. Launched 28 May 1965, the mission resulted in failure when its Atlas booster exploded two minutes after launch.

OV1-2 US Air Force satellite

Orbiting Vehicle 1-2, launched 5 October 1965, was the third, and first successful, satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. A radiation measuring satellite designed to conduct research for the planned Manned Orbital Laboratory project, OV1-2 was the first American spacecraft to be placed into orbit on a western trajectory. The satellite stopped functioning in April 1967 after a series of technical problems starting two months after launch.

LES-3 Former communications satellite

Lincoln Experimental Satellite 3, also known as LES-3, was a communications satellite, the third of nine in the Lincoln Experimental Satellite. Launched by the United States Air Force (USAF) on 21 Dec 1965, it was stranded in a Geostationary Transfer Orbit rather than its planned circular high orbit. Despite this, LES-3 returned good data on communications propagation in the UHF band.

LES-4 Former communications satellite

Lincoln Experimental Satellite 4, also known as LES-4, was a communications satellite, the fourth of nine in the Lincoln Experimental Satellite, and the first of the series designed for operations at geosynchronous altitudes. Launched by the United States Air Force (USAF) on 21 December 1965, it demonstrated many then-advanced technologies including active use of the military's SHF band to service hundreds of users.

OV1-4 US Air Force satellite

Orbiting Vehicle 1-4, launched 30 Mar 1966, was the fourth, and second successful, satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-4 was a long-term bioscience and materials science satellite, designed to return data relevant to long-term human presence in space. Its launch marked the first time two satellites were placed into orbit side-by-side with each other.

OV1-5 US Air Force satellite

Orbiting Vehicle 1-5 was launched 30 Mar 1966, and was the fifth satellite in the OV1 series of the United States Air Force's Orbiting Vehicle program. OV1-5 conducted optical experiments, surveying the Earth in the infrared spectrum to see if water, land, mountains and deserts could be distinguished by their thermal gradients. It was launched concurrently with OV1-4 in the first ever side-by-side satellite orbital deployment.

OV3-1 US Air Force satellite

Orbiting Vehicle 3-1, launched 22 April 1966, was the first satellite in the OV3 series of the United States Air Force's Orbiting Vehicle program. The satellite measured radiation above the Earth, returning useful data for over a year. It is still in orbit as of 1 April 2021.

Initial Defense Communications Satellite Program American satellite family

The Initial Defense Communications Satellite Program or IDCSP was the first United States Department of Defense communications satellite constellation and the first stage of the Defense Communications Satellite Program (DCSP). Launched in five groups by Titan IIIC launch vehicles to near equatorial, subsynchronous orbits between 1966 and 1968, they were intended to be experimental testbeds. They were so successful that, by the time of the launch of the last set of eight satellites, the IDCSP was deemed operational and renamed Initial Defense Satellite Communications System or IDSCS. This system allowed real-time collection of battlefield intelligence during the Vietnam War. A total of 35 IDCSP satellites were launched, 27 successfully.

OV3-4 US Air Force satellite

Orbiting Vehicle 3-4, launched 10 June 1966, was the second satellite to be launched in the OV3 series of the United States Air Force's Orbiting Vehicle program. The satellite measured radiation above the Earth, helping to determine the hazard posed to human spaceflight at typically traveled altitudes. OV3-4 is still in orbit as of 6 June 2021.

OV2-5 US Air Force satellite

Orbiting Vehicle 2-5, the third and last satellite of the second series of the United States Air Force's Orbiting Vehicle program, was an American particle science and ionosphere research satellite. Launched 26 September 1968 along with three other satellites, OV2-5 became the first scientific satellite to operate at geosynchronous altitude.

References

  1. 1 2 McDowell, Jonathan. "Launch Log". Jonathan's Space Report. Retrieved November 26, 2020.
  2. 1 2 "OV2-3". NASA Space Science Data Coordinated Archive. Retrieved 26 November 2020.
  3. 1 2 3 4 5 6 7 8 Powell, Joel W.; Richards, G.R. (1987). "The Orbiting Vehicle Series of Satellites". Journal of the British Interplanetary Society. Vol. 40. London: British Interplanetary Society.
  4. 1 2 3 "OV2-1A Readied for Titan 3 A Test" . Aviation Week and Space Technology. New York: McGraw Hill Publishing Company. February 8, 1965. Retrieved February 10, 2020.
  5. "OV2-1". NASA Space Science Data Coordinated Archive. Retrieved February 10, 2020.
  6. 1 2 3 4 5 "Titan 3 Transtage Malfunctions, Fails to Achieve Circular Orbit" . Aviation Week and Space Technology. New York: McGraw Hill Publishing Company. 27 December 1965. p. 27. Retrieved 24 November 2020.
  7. "OV2-3" . Retrieved 26 November 2020.
  8. Krebs, Gunter. "OV2". Gunter's Space Page. Retrieved February 12, 2019.