| astronautix.com | July 07 |
1914 - Nation: USA.
Goddard receives US Patent 1,102,653, covering the concept of using multiple rocket stages to achieve high velocities. References: 377 .
1943 - Nation: Germany. Launch Vehicle: V-2.
Adolf Hitler gave the German V-2 program highest military priority. References: 17 .
1946 - Nation: USA.
1948 - Nation: USSR.
Decree 256 'On establishment of NII Branch No 7 to ground test rocket engines' was issued. References: 474 .
1954 - Nation: USSR. Launch Vehicle: R-1.
1959 - Nation: USA. Launch Site: Wallops Island . Launch Vehicle: Argo.
Four-stage Argo D4 rocket with an ARDC Javelin payload fired from Wallops Island to an altitude of 750 miles, first in a series of USAF-NASA launchings to measure natural radiation surrounding the earth. References: 17 .
1960 - Nation: USA.
1961 - Nation: USA. Launch Vehicle: Saturn V.
The NASA Administrator and the Secretary of Defense concluded an agreement to study development of large launch vehicles for the national space program. For this purpose, the DOD-NASA Large Launch Vehicle Planning Group was created, reporting to the Associate Administrator of NASA and to the Assistant Secretary of Defense (Deputy Director of Defense Research and Engineering). References: 16 .
1961 - Nation: USA. Launch Vehicle: Atlas Centaur.
Walter F. Burke of McDonnell summarized the company's studies of the redesigned Mercury spacecraft for Space Task Group's senior staff. McDonnell had considered three configurations: (1) the minimum-change capsule, modified only to improve accessibility and handling, with an adapter added to carry such items as extra batteries; (2) a reconfigured capsule with an ejection seat installed and most of the equipment exterior to the pressure vessel on highly accessible pallets; and (3) a two-man capsule, similar to the reconfigured capsule except for the modification required for two rather than one-man operation. The capsule would be brought down on two Mercury-type main parachutes, the ejection seat serving as a redundant system. In evaluating the trajectory of the two-man capsule, McDonnell used Atlas Centaur booster performance data.
1966 - Nation: USA.
In a memorandum to Headquarters staff members, Advanced Manned Missions Program Director Edward Z. Gray summarized the three separate study efforts underway within NASA directed toward evaluating the S-IVB stage as a manned laboratory: (1) The spent-stage experiment support module (SSESM) study, a joint effort by MSC and MSFC. (2) A spent S-IVB-stage utilization study at MSFC. (3) A Saturn V single-launch space station. Additional Details: Three separate study efforts within NASA evaluating the S-IVB stage as a manned laboratory..
1970 - Nation: USA.
1970 - - 10:33 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Voskhod 11A57.
High resolution photo reconnaissance satellite; returned film capsule References: 1 , 2 , 6 .
1972 - - 17:46 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC4E. Launch Vehicle: Titan 3D. LV Configuration: Titan 3D s/n 23D-5.
Radar monitoring. References: 1 , 2 , 5 , 6 , 172 .
KH-9 type satellite. Investigation of the upper atmosphere and outer space. References: 1 , 2 , 5 , 6 .
1977 - - 07:26 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Vostok 8A92M.
1978 - Nation: USA.
1978 - Nation: USA.
Complete mate forward and aft payload bay doors, Columbia (OV-102) References: 15 .
1978 - - 11:26 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC31. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n S15000-128.
Unmanned supply vessel to Salyut 6. Delivery of fuel, consumable materials and equipment to the Salyut 6 station. Docked with Salyut 6 on 9 Jul 1978 12:58:59 GMT. Undocked on 2 Aug 1978 04:57:44 GMT. Destroyed in reentry on 4 Aug 1978 01:31:07 GMT. Total free-flight time 3.92 days. Total docked time 23.67 days. References: 1 , 2 , 6 , 275 .
1981 - - 12:28 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Soyuz 11A511U.
Photo surveillance; returned film capsule. References: 1 , 2 , 6 .
1982 - - 09:50 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 65093-473.
Military navigation satellite. Replaced Cosmos 1225. References: 1 , 2 , 5 , 6 .
1987 - - 22:04 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 53796-177.
Military navigation satellite. References: 1 , 2 , 5 , 6 .
1988 - - 08:09 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC16/2. Launch Vehicle: Soyuz 11A511U.
Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation. References: 1 , 2 , 6 .
1988 - - 17:38 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC200L. Launch Vehicle: Proton 8K82K / 11S824F. LV Configuration: Proton 8K82K s/n 356-02 / 11S824F s/n 2L.
Second of two missions to Mars' moon Phobos; carried 2 landers; planned to enter Mars orbit. Phobos 1 operated nominally until an expected communications session on 2 September 1988 failed to occur. The failure of controllers to regain contact with the spacecraft was traced to an error in the software uploaded on 29/30 August which had deactivated the attitude thrusters. This resulted in a loss of lock on the Sun, resulting in the spacecraft orienting the solar arrays away from the Sun, thus depleting the batteries. Left in solar Orbit (Heliocentric). References: 1 , 2 , 5 , 6 , 67 , 118 , 274 , 296 .
1991 - - 02:32 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17A. Launch Vehicle: Delta 7925. LV Configuration: Delta 7925 / Delta s/n 206.
Test flight of DOD sensors; Low Altitude Satellite Experiment. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2 , 5 , 6 .
Global Positioning System. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 1 , 2 , 5 , 6 .
1992 - - 09:21 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17B. Launch Vehicle: Delta 7925. LV Configuration: Delta 7925 / Delta s/n 211.
Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
1993 - - 07:12 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC90. Launch Vehicle: Tsyklon 2.
Third launch of new EORSAT, final of three stationed at 120 degree intervals on the same orbit with a 0 degree ascending node. Ocean surveillance. References: 1 , 2 , 5 , 6 , 69 .
1995 - - 16:23 GMT. Nation: Spain. Launch Site: Kourou . Launch Complex: ELA2. Launch Vehicle: Ariane 4. LV Configuration: Ariane 40 s/n V75.
Universidad Politecnia de Madrid Satellite; experimental communications, microgravity experiments. References: 2 , 5 , 6 .
Caracterisation de l'Environnement Radioelectrique par un Instrument Spatiale Embarque; examined Earth RF environment. Customer: Alcatel Espace/DME. French government research payload incorporated into an advance microsatellite platform. Still operational as of 2000. References: 2 , 5 , 6 .
1998 - Nation: Israel. Launch Site: Barents Sea . Launch Complex: Sub K407. Launch Vehicle: Shtil-1/1N. LV Configuration: .
The first satellite launch from a submarine. The Shtil-1 launch vehicle was a converted R-29RM (RSM-54) three stage liquid propellant submarine launched ballistic missile made by the Makeyev design bureau. The satellite payload is placed in the standard R-29RM reentry vehicle. The launch plaform was the K-407 Novomoskovsk, a 667BDRM Delfin class submarine of the Russian Northern Fleet's 3rd Flotilla. Launch was from the Barents Sea at 69.3 degrees N x 35.3 degrees E. The Shtil contained an Israeli instrument package. References: 279 .
The first satellite launch from a submarine. The Shtil-1 launch vehicle was a converted Makeyev R-29RM SLBM. The satellite payload was placed in the standard re-entry vehicle. The launch platform was the K-407 Novomoskovsk, a 667BDRM Delfin class submarine of the Russian Northern Fleet 3rd Flotilla. The launch was made from a firing range in the Barents Sea off the coast of the Kolskiy Peninsula, at 35.3 deg E 69.3 deg N. The payloads were the Tubsat-N and Tubsat-N1 `nanosatellites'. Tubsat-N entered a 400 x 776 km x 78.9 deg orbit. Both carried small store-forward communications payloads used to keep track of transmitters placed on vehicles, migrating animals, and marine buoys. They are owned, operated and built by the Technische Universitat Berlin (TUB).