1959 April 1 - -
Two-man Mercury capsule proposed. Nation: USA. Spacecraft: Gemini. H. Kurt Strass of the Space Task Group (STG) at Langley Field, Virginia described some preliminary ideas of STG planners regarding a follow-on to Mercury: (1) an enlarged Mercury capsule to place two men in orbit for three days; (2) a two-man Mercury capsule and a large cylindrical structure to support a two-week mission. (In its 1960 budget, NASA had requested $2 million to study methods of constructing a manned orbiting laboratory or converting the Mercury spacecraft into a two-man laboratory for extended space missions.)
Additional Details: Two-man Mercury capsule proposed..
1959 April 1 - Launch Vehicle: Soyuz. Model: R-7A. -
R-7A ICBM production approved. Nation: USSR. Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On production of the R-7A missile at Plant No. 1001 at Krasnoyarsk-26 and establishment of a branch' was issued. References: 474.
1959 April - -
Mercury parachute design unsafe for operation. Nation: USA. Program: Mercury. Spacecraft: Mercury. In the recovery landing system, the extended-skirt main parachute was found to be unsafe for operation at altitudes of 10,000 feet and was replaced by a 'ring-sail' parachute of similar size. This decision was made after a drop when the main parachute failed to open and assumed a 'squidding' condition. Although little damage was sustained by the spacecraft on water impact, parachute experts decided that the ring-sail configuration should be adopted, and the air drop spacecraft were fitted.
References: 483.
1959 April - Launch Vehicle: Atlas. Model: Atlas E. -
Scheduled design complete (95%) for Atlas E-series missiles Nation: USA. References: 4460.
1959 April 1-8 - -
Goett Committee to study advanced manned space flight missions Nation: USA. Program: Apollo. John W. Crowley, Jr., NASA Director of Aeronautical and Space Research, notified the Ames, Lewis, and Langley Research Centers, the High Speed Flight Station (later Flight Research Center), the Jet Propulsion Laboratory, and the Office of Space Flight Development that a Research Steering Committee on Manned Space Flight would be formed. Harry J. Goett of Ames was to be Chairman of the Committee, which would assist NASA Headquarters in carrying out its responsibilities in long-range planning and basic research on manned space flight.
References: 16.
April 1959 - Launch Vehicle: DF-1. -
Chinese/Russian missile talks Nation: China. A Chinese delegation goes to Russia to discuss delivery of more tooling and machine tools for missile production.
1959 April 2 - -
Seven astronauts selected for Mercury project. Nation: USA. Program: Mercury. Class: Manned. Type: Spacecraft. Spacecraft: Mercury. Seven astronauts were selected for Project Mercury after a series of the most rigorous physical and mental tests ever given to U.S. test pilots. Chosen from a field of 110 candidates, the finalists were all qualified test pilots: Capts. Leroy G. Cooper, Jr., Virgil I. Grissom, and Donald K. Slayton, (USAF); Lt. Malcolm S. Carpenter, Lt. Comdr. Alan B. Shepard, Jr., and Lt. Comdr. Watler M. Schirra, Jr. (USN); and Lt. Col. John H. Glenn (USMC).
References: 17.
1959 April 2 - -
Bidders briefing for Project Mercury worldwide tracking range Nation: USA. Program: Mercury. A preliminary briefing was conducted for prospective bidders on construction of the worldwide tracking range for Project Mercury. This meeting was attended by representatives from 20 companies. At this time the preliminary plan called for an orbital mission tracking network of 14 sites. Contacts had not been made with the governments of any of the proposed locations with the exception of Bermuda. It was planned that all the sites would have facilities for telemetry, voice communications with the pilot, and teletype (wire or radio) communications with centers in the United States for primary tracking. The tracking sites would provide the control center at Cape Canaveral, Florida, with trajectory predictions; landing-area predictions; and vehicle, systems, and pilot conditions.
References: 483.
1959 April 2 - -
NASA Astronaut Training Group 1 selected. Nation: USA. The group was selected to provide six pilots for the single-crew Mercury manned spacecraft. Originally a wide pool of candidates was going to be considered, but in December 1958 President Eisenhower ruled that military test pilots would form the candidate pool.. Qualifications: Qualified jet pilot with minimum 1,500 flight-hours/10 years experience, graduate of test pilot school, bachelor's degree or equivalent, under 40 years old, under 180 cm height, excellent physical condition.. Screening of military service records showed 110 military officers that met these criteria. These 110 were to be called in three groups for briefings on the Mercury program. Of the first two groups of 35 called, 56 volunteered for further physical and psychiatric tests. This provided enough candidates and the third group was never even called for a briefing or asked if they would like to volunteer. Of the 56 tested, seven were finally selected (no objective way was found to reduce the seven finalists to six).
Of the seven astronauts, all eventually flew in space. Grounded due to a heart murmur, Slayton had to wait 16 years for his flight aboard the last Apollo mission. Glenn left for a career in politics after becoming the first American to orbit the earth, but returned to space aboard a shuttle over 36 years later in a NASA publicity stunt. Schirra was the only astronaut to fly aboard Mercury, Gemini, and Apollo spacecraft. Shepard was the only one to reach the lunar surface (after being grounded for a medical condition during the Gemini program). Grissom would die in the Apollo 204 ground fire.
1959 April 2-16 - Launch Vehicle: Little Joe. -
Project Mercury animal payload program. Nation: USA. Program: Mercury. Spacecraft: Mercury. NASA and the military services conducted meetings to draft final plans for the Project Mercury animal payload program. The animal program was planned to cover nine flights, involving Little Joe, Redstone, Jupiter, and Atlas launch vehicles. References: 483.
1959 April 2-5 - -
Advanced manned space program to follow Project Mercury Nation: USA. Program: Apollo. Spacecraft: Mercury. The advanced manned space program to follow Project Mercury was discussed at a NASA Staff Conference held in Williamsburg, Va. Three reasons for such a program were suggested: - Preliminary step to development of spacecraft for manned interplanetary exploration.
- Extended duration work in the space environment.
- Support of the military space mission.
Among areas requiring study were the cost of an equatorial launch site, adequacy of tracking stations and DOD-NASA coordination of tracking systems, and the need for NASA's own propulsion test stands and facilities.
References: 16.
1959 April 3 - 17:11 GMT - Launch Site: Cape Canaveral. Launch Complex: LC15. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I A-4. -
Test mission Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi). References: 2.
1959 April 4 - Launch Site: AMR DZ. Launch Complex: -. Launch Pad: 29.0 N x 79.0 W. Launch Vehicle: Bold Orion. Model: Bold Orion 2. LV Configuration: Bold Orion-2. -
Interceptor mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1959 April 4 - 00:34 GMT - Launch Site: Cape Canaveral. Launch Complex: LC26B. Launch Pad: -. Launch Vehicle: Jupiter. LV Configuration: Jupiter IRBM CM-22A. -
Research and development test Nation: USA. Agency: USAF/ABMA. Apogee: 500 km (310 mi). Fired from AMR at 1934 hours EST. The primary mission of impacting a nose cone in a pre-calculated target area (MILS Network) was successfully accomplished with an impact of 0.8 nm under end 5.0 nm to the left of the 1,302 nm range. The lateral miss was believed to have been caused by a drifting gyro.
References: 2.
1959 April 7 - Launch Vehicle: RS. -
NM-1 first flight Nation: USSR. A subsonic aerodynamic test vehicle of the RSR trisonic missile, the NM-1 was first flown oby test p[ilot Amert-Khan Sultan.
1959 April 7 - 14:46 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AA3.160C. FAILURE: Failure. -
Aeronomy mission Nation: USA. Agency: USAF. Apogee: 317 km (196 mi). References: 2.
1959 April 8 - 06:35 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Able II. LV Configuration: Thor Able II 133. -
RVX-1 Reentry test / particles mission Nation: USA. Agency: USAF. Apogee: 1,230 km (760 mi). References: 2.
1959 April 9 - -
First group of US astronauts announced Nation: USA. Program: Mercury. Spacecraft: Mercury. At a press conference in Washington, D.C., NASA Administrator T. Keith Glennan announced the seven pilots had been selected for the Mercury program. References: 16.
1959 April 9-10 - -
Escape configurations for Mercury spacecraft Nation: USA. Program: Mercury. Spacecraft: Mercury. Investigations of two escape configurations for Mercury spacecraft were conducted in a 16-foot transonic circuit at the Arnold Engineering Development Center, Tullahoma, Tennessee, for determination of static stability and drag characteristics of the configurations.
References: 483.
1959 April 10 - -
Mercury escape-motor canting-angle tests completed at Wallops Island. Nation: USA. Program: Mercury. Spacecraft: Mercury. Escape-motor canting-angle tests were completed at Wallops Island. Tests were conducted in 5 degree increments between 10 degrees to 30 degrees, and visually it appeared stability was better at the larger angle. References: 483.
1959 April 12 - -
Mercury impact tests Nation: USA. Program: Mercury. Spacecraft: Mercury. Tests were in progress at Langley in which an aluminium honeycomb structure was used partially to absorb the spacecraft impact load. Robert R. Gilruth, Project Mercury Director, had stated his belief of this requirement on January 16, 1959. References: 483.
1959 April 12 - -
Space Task Group conducted the second full-scale Mercury beach abort test on Wallops Island. Nation: USA. Program: Mercury. Spacecraft: Mercury. A deliberate thrust misalignment of 1 inch was programed into the escape combination. Lift-off was effected cleanly, and a slow pitch started during the burning of the escape rocket motor. The tower separated as scheduled and the drogue and main parachutes deployed as planned. The test was fully successful.
References: 483.
1959 April 13 - -
Mercury small-scale escape-tower combinations launched Nation: USA. Program: Mercury. Spacecraft: Mercury. Two small-scale spacecraft escape-tower combinations were launched successfully at Wallops Island. On the next day a full-scale spacecraft escape system was launched. The complete sequence of events - escape system firing, escape tower jettisoning, parachute deployment, landing, and helicopter recovery - was satisfactory.
References: 483.
1959 April 13 - 21:18 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena A. LV Configuration: Thor Agena A 170 / Agena A 1018. -
Discoverer 2 Nation: USA. Payload: KH-1 prototype / Agena A 1022. Mass: 743 kg (1,638 lb). Class: Surveillance. Type: Military. Spacecraft: KH-1. Agency: DARPA. Perigee: 239 km (148 mi). Apogee: 346 km (214 mi). Inclination: 89.90 deg. Period: 90.40 min. COSPAR: 1959-Gamma-1. USAF Sat Cat: 14. Decay Date: 1959-04-26. KH-1 prototype; tested capsule recovery techniques; did not carry camera; capsule recovery failed. Because of a timing error, the US believed that the capsule landed somewhere on the island of Spitsbergen, north of Norway, instead of landing in the recovery zone near Hawaii. The capsule was never found; and CIA officials suspect it may have been snatched by the Soviets. The search for this capsule formed the basis of the book and film 'Ice Station Zebra'.In the winter of 1960/1961, a US Discovery spy satellite capsule was found by loggers near Kalinin, 200 km north of Moscow. The loggers cracked it open with an axe. Sergei Khrushchev believed this to be the Discoverer 2 capsule. What was left was examined by Soviet engineers but didn’t reveal much information - it was a polished aluminium sphere, 30 cm in diameter, gilded on the exterior. Some said it was found as early as the winter of 1959.
References: 2, 6.
1959 April 14 - 02:49 GMT - Launch Site: Cape Canaveral. Launch Complex: LC18A. Launch Pad: LC18A. Launch Vehicle: Vanguard. Model: Vanguard. LV Configuration: Vanguard SLV-5. FAILURE: Stage 2 damaged at separation. -
Vanguard 3A Nation: USA. Program: Vanguard. Payload: Magnetometer satellite. Mass: 10 kg (22 lb). Class: Earth. Type: Magnetosphere. Spacecraft: Vanguard 3. Agency: NASA. Apogee: 100 km (60 mi). COSPAR: F590414A. Decay Date: 1959-04-13. References: 126.
-
30-inch Sphere Nation: USA. Program: Vanguard. Payload: Air density satellite. Spacecraft: Vanguard 3. Agency: USN. Apogee: 100 km (60 mi). COSPAR: F590414B. References: 279.
1959 April 14 - 21:46 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 3D. FAILURE: Failure. -
Research and development launch Nation: USA. Agency: USAF. Apogee: 1.00 km (0.60 mi). References: 2.
1959 April 15 - Launch Vehicle: Saturn I. Model: Saturn A-1. -
Use of Titan for Saturn upper stages Nation: USA. Program: Apollo. In response to a request by the DOD-NASA) Saturn Ad Hoc Committee, the Army Ordnance Missile Command (AOMC) sent a supplement to the "Saturn System Study" to the Advanced Research Projects Agency ARPA describing the use of Titan for Saturn upper stages.
Additional Details: Use of Titan for Saturn upper stages. References: 16.
1959 April 16 - -
TF-102B and T-33 aircraft for Project Mercury astronauts. Nation: USA. Program: Mercury. NASA requested that the Air Force furnish two TF-102B and two T-33 aircraft to be used by the Project Mercury astronauts. One of the requirements in the astronaut training program was to maintain proficiency in high performance aircraft. References: 483.
1959 April 16 - 20:46 GMT - Launch Site: Vandenberg. Launch Complex: LE-8. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DM-18A. LV Configuration: Thor DM-18A 161. -
IWST test flight Nation: USA. Agency: RAF. Apogee: 520 km (320 mi). Integrated Weapon System Training 1. First Thor IRBM launched by British crew at Vandenberg AFB. References: 2.
1959 April 19 - Launch Site: Kapustin Yar. Launch Complex: VLAD. Launch Pad: -. Launch Vehicle: Burya. LV Configuration: Burya 2-05. -
Burya flight 11 Nation: USSR. Agency: SSSR. Apogee: 17 km (10 mi). Launched after prior 20 Februry flight attempt. The suspect booster was replaced. Successful flight lasting T+33.5 minutes, achieving a range of 1,766 km and a speed of Mach 3.15 at 17.0 km altitude. References: 2.
1959 April 20 - -
Canada-NASA sounding rocket agreement. Nation: Canada. NASA announced acceptance of proposals by the Canadian Defense Research Telecommunications Establishment for continuing joint rocket and satellite ionospheric experiments of a nonmilitary nature. References: 17.
1959 April 20 - 15:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris AX. LV Configuration: Polaris AX-6. -
Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1959 April 21 - 01:05 GMT - Launch Site: Holloman. Launch Complex: A. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AA3.181C. -
Ionosphere mission Nation: USA. Agency: USAF. Apogee: 235 km (146 mi). References: 2.
1959 April 22 - -
Tower configuration best escape system for the Mercury spacecraft. Nation: USA. Program: Mercury. Spacecraft: Mercury. In a meeting at Langley, NASA officials concluded that the tower configuration was the best escape system for the Mercury spacecraft and development would proceed using this concept. However, limited studies of alternate configurations would continue. References: 483.
1959 April 23 - Launch Site: Grand Turk Island DZ. Launch Complex: -. Launch Pad: -. Launch Vehicle: Hound Dog. LV Configuration: Hound Dog 001. -
Hound Dog Test mission Nation: USA. Program: Navaho. Agency: USAF. Apogee: 20 km (12 mi). First Hound Dog test launch. References: 2, 872.
1959 April 23 - 05:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DM-18A. LV Configuration: Thor DM-18A 176. -
Series IV research and development launch Nation: USA. Agency: USAF. Apogee: 520 km (320 mi). Fourth recovery of a data capsule at AMR, USAF Thor 1,500-mile accuracy test flight. References: 2.
1959 April 24 - -
All three military services studying a base on the moon Nation: USA. Spacecraft: Lunex Lunar Expedition, Horizon Lunar Outpost, Navy SLV. Testifying before the Senate Committee on Aeronautical and Space Sciences, Maj. Gen. Bernard A. Schriever, Commander of the Air Force Ballistic Missile Division, stated that all three military services should be studying the possibility of a base on the moon. Up to that point, he felt, all such studies had been "in the blue thinking."
References: 16.
1959 April 25 - 05:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC18B. Launch Pad: LC18B. Launch Vehicle: Delta. Model: Thor DM-18A. LV Configuration: Thor DM-18A 164. -
Series IV research and development launch Nation: USA. Agency: USAF. Apogee: 520 km (320 mi). References: 2.
1959 April 27 - -
Mercury search and rescue procedures developed. Nation: USA. Program: Mercury. Class: Manned. Type: Spacecraft. Spacecraft: Mercury. Meeting of DOD working group on Project Mercury search and recovery operations was held at Patrick Air Force Base, with major emphasis placed on the first two ballistic Atlas shots, and command relationships. References: 17, 278.
1959 April 27 - -
Project Mercury astronauts reported for duty Nation: USA. Program: Mercury. The seven Project Mercury astronauts reported for duty. A tentative schedule of Mercury astronaut activities for the first months of training was issued. Actual training began the next day. Within 3 months the astronauts were acquainted with the various facets of the Mercury program. The first training week was as follows: Monday, April 27, check in; April 28, general briefing; April 29, spacecraft configuration and escape methods; April 30, support and restraint; May 1, operational concepts and procedures. These lectures were presented by specialists in the particular field of study. Besides the above, unscheduled activities involved 3 hours flying time and 4 hours of athletics.
References: 483.
1959 April 27 - -
Project Mercury was accorded the DX priority procurement rating. Nation: USA. Program: Mercury. Spacecraft: Mercury. References: 483.
1959 April 27 - Launch Site: Cape Canaveral. Launch Complex: LC10. Launch Pad: -. Launch Vehicle: Draco. FAILURE: Failure. -
Test mission Nation: USA. Agency: USAF. Apogee: 0 km ( mi). References: 2.
1959 April 28 - Launch Vehicle: Delta. Model: Delta A. -
Delta launch vehicle contract. Nation: USA. NASA announced the signing of a $24 million contract with Douglas Aircraft Co., Inc., for a three-stage Thor-Vanguard launching rocket called Delta. References: 17.
1959 May 1 - -
Goddard Space Flight Center established. Nation: USA. NASA's Administrator announced the naming of Goddard Space Flight Center under construction near Greenbelt, Md., in commemoration of Robert H. Goddard, American pioneer in rocket research. Dr. Harry J. Goett was appointed Director in September. STG was transferred to the authority of the newly formed Goddard Space Flight Center but remained based at Langley Field, Va.
References: 17.
1959 May 1 - Launch Vehicle: Saturn I. -
Unmanned Lunar Soft Landing Vehicle Nation: USA. Program: Apollo. Spacecraft: Surveyor. The Army Ordnance Missile Command submitted to NASA a report entitled "Preliminary Study of an Unmanned Lunar Soft Landing Vehicle," recommending the use of the Saturn booster. References: 16.
1959 May 1 - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Long Tom. -
Test mission Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi). References: 2.
1959 May 1 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier ASROC Cajun. LV Configuration: Terrier ASROC Cajun Terasca. FAILURE: Failure. -
Test mission Nation: USA. Agency: USN. Apogee: 0 km ( mi). References: 2.
1959 May 2 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Antares. Model: OPd-56-39-22D. LV Configuration: OPd-56-39-22D 001. -
Re-entry Vehicle test Nation: France. Agency: ONERA. Apogee: 150 km (90 mi). References: 2.
1959 May 3 - Launch Vehicle: Saturn I. -
First H-1 engine for the Saturn delivered Nation: USA. Program: Apollo. The first Rocketdyne H-1 engine for the Saturn arrived at the Army Ballistic Missile Agency (ABMA ). The H-1 engine was installed in the ABMA test stand on May 7, first test-fired on May 21, and fired for 80 seconds on May 29. The first long-duration firing - 151.03 seconds - was on June 2.
References: 16.
1959 May 4 - 18:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC15. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I A-6. -
Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi). Successful dummy second stage separation. References: 2.
1959 May 5 - 01:45 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee AJ10-34. LV Configuration: Aerobee AJ10-34 AA2.141C. -
Aeronomy mission Nation: USA. Agency: USAF. Apogee: 132 km (82 mi). References: 2.
1959 May 6 - -
Jastrow Committee on lunar exploration created. Nation: USA. Program: Apollo. NASA created a committee to study problems of long-range lunar exploration to be headed by Dr. Robert Jastrow. References: 17, 27.
1959 May 6 - Launch Vehicle: Little Joe. -
Pigs not to fly in space in Project Mercury Nation: USA. Program: Mercury. Spacecraft: Mercury. Pigs were eliminated as Little Joe flight test subjects when studies disclosed that they could not survive long periods of time on their backs. However, McDonnell did use a pig, 'Gentle Bess,' to test the impact crushable support, and the test was successful.
References: 483.
1959 May 7 - -
USAF System Requirement 201 (Dyna-Soar) Nation: USA. Spacecraft: Dynasoar. ARDC headquarters issued System Requirement 201, declaring the purpose of the Dyna-Soar vehicle was to determine the military potential of a boost-glide weapon system and provide research data on flight characteristics up to and including global flight. The Air Force disagreed with the position of the Secretary of Defence's office that Dynasoar be limited to suborbital research flights.
1959 May 7 - 01:47 GMT - Launch Site: Cape Canaveral. Launch Complex: LC26B. Launch Pad: -. Launch Vehicle: Jupiter. LV Configuration: Jupiter IRBM AM-12. -
Research and development test / ionosphere mission Nation: USA. Agency: USAF/ABMA. Apogee: 500 km (310 mi). Fired from AMR at 2047 hours EST. All primary missions were essentially successful, although the impact was 69 nm short and 4.9 nm to the right of the 1,302 nm predicted impact point. This undershoot was due to thrust controller deviation which commanded the exceedingly high thrust level during the main power flight pre-selected flight path. Cut-off occurred at 144 seconds of flight.
References: 2.
1959 May 8 - 19:28 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris AX. LV Configuration: Polaris AX-8. -
Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1959 May 9 - Launch Vehicle: Atlas. Model: Atlas Vega. -
High-resolution photographs of the moon using Vega rocket Nation: USA. Program: Apollo. Spacecraft: Lunar Orbiter. Milton W. Rosen of NASA Headquarters proposed a plan for obtaining high-resolution photographs of the moon. A three-stage Vega would place the payload within a 500-mile diameter circle on the lunar surface. A stabilized retrorocket fired at 500 miles above the moon would slow the instrument package sufficiently to permit 20 photographs to be transmitted at a rate of one picture per minute.
Additional Details: High-resolution photographs of the moon using Vega rocket. References: 16.
1959 May 9 - 18:59 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7. LV Configuration: R-7 No. IZ-21. FAILURE: Failure. -
GCh No. 17 (III) test Nation: USSR. Agency: MVS. Apogee: 1,000 km (600 mi). R-7 development test flight. (GCh No. 17 (III)) References: 2.
1959 May 10 - Launch Vehicle: R-5. Model: R-5M. -
First extended field deployment of a nuclear Soviet IRBM Nation: USSR. The first extended field deployment of the R-5M from a field location was undertaken during Army exercises at Simferopol. This was the first field deployment with nuclear weapons in Soviet history and verified the ability of the ballistic missile systems to operate in an integrated manner with the ground forces. The R-5M was formally accepted into military service in 1960. The missile continued in service until 1968.
1959 May 12 - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: ALA3. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 1013. FAILURE: Known initial laying error of approximately 26 min. -
Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Missile test failure. Missed aimpoint by 1,091 m. References: 2.
1959 May 12 - 11:39 GMT - Launch Site: Holloman. Launch Complex: A. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AA3.200C. -
Aeronomy mission Nation: USA. Agency: USAF. Apogee: 145 km (90 mi). References: 2.
1959 May 12 - 17:35 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DM-18A. LV Configuration: Thor DM-18A 187. -
Series IV research and development launch Nation: USA. Agency: USAF. Apogee: 520 km (320 mi). References: 2.
1959 May 13 - Launch Vehicle: R-16, R-9. -
R-9 and R-16 development measures approved. Nation: USSR. Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On start of dedicated work on the R-9 and R-16 ICBMs' was issued. References: 474.
1959 May 13 - -
NII-88 Computer Centre created. Nation: USSR. Decree 'On creation of the Computer Centre of NII-88' was issued. References: 474.
1959 May 14 - 05:52 GMT - Launch Site: Cape Canaveral. Launch Complex: LC5. Launch Pad: -. Launch Vehicle: Jupiter. LV Configuration: Jupiter IRBM AM-17. -
Research and development test / ionosphere mission Nation: USA. Agency: USAF/ABMA. Apogee: 500 km (310 mi). Fired from AMR at 0052 hours EST to test impact accuracy. This shot may be considered as having hit the target. The impact was: .26 nm over and 0.4 nm to the left of the predicted point of impact. Accuracy of the MILS Network was approximated at plus-or-minus 0.25 nm. All primary and secondary missions were accomplished except for photographic recording of the second separation. This could not be accomplished because of the firing date.
References: 2.
1959 May 15 - Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan 1 B-4. FAILURE: Exploded during static testing. -
Titan 1 B-4 Nation: USA. References: 2.
1959 May 16 - Launch Site: Cuxhaven. Launch Complex: -. Launch Pad: -. -
First DRG Rocket Mail Nation: Germany. First launches from Arensch to Berensch of DRG (German Rocket Society) 'postcard rockets'. 100 would be launched in the next two years. Ten launches were made carrying 5000 postcards. The subsonic 5 kg rockets were 2 m long, produced 50 kgf thrust, were recovered under three or four parachutes, and had an average accuracy of 130 m over a 3 km range.
1959 May 17 - -
Scale model of Mercury for launch from Wallops Island to mach 18. Nation: USA. Program: Mercury. Spacecraft: Mercury. The Langley Research Center was in the process of preparing a one-fourteenth scale model of the Mercury spacecraft for launch from Wallops Island on a five-stage rocket to a speed of mach 18. References: 483.
1959 May 17 - -
PKA Spaceplane Draft Project Nation: USSR. Spacecraft: PKA. Tsybin’s design was called the gliding spacecraft (PKA). The draft project, undertaken in co-operation with Korolev’s OKB-1, was signed by Tsybin on 17 May 1959.The piloted PKA would be inserted into a 300 km altitude orbit by a Vostok launch vehicle. After 24 to 27 hours of flight the spacecraft would brake from orbit, gliding through the dense layers of the earth’s atmosphere. At the beginning of the descent, in the zone of most intense heating, the spacecraft would take advantage of a hull of original shape (called ‘Lapotok’ by Korolev after the Russian wooden shoes that it resembled). After braking to 500 to 600 m/s at an altitude of 20 km, the PKA would glide to a runway landing on deployable wings, which would move to a horizontal position from a stowed vertical position over the back of the spacecraft. Control of the PKA in flight was by rocket jets or aerodynamic surfaces, depending on the phase of flight.
1959 May 19 - 04:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC14. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 7D. FAILURE: Failure. -
Research and development launch Nation: USA. Agency: USAF. Apogee: 1.00 km (0.60 mi). References: 2.
1959 May 21 - -
Specifications for Tracking and Ground Instrumentation System for Project Mercury Nation: USA. Program: Mercury. Langley Specification Number S-45, entitled 'Specifications for Tracking and Ground Instrumentation System for Project Mercury,' was issued. Proposals were received from seven contractor teams by June 22, 1959, and technical evaluations were started. References: 483.
1959 May 21 - 06:40 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Able II. LV Configuration: Thor Able II 135. -
RVX-1 Re-entry Vehicle test Nation: USA. Agency: USAF. Apogee: 520 km (320 mi). References: 2.
1959 May 22 - -
Production of Vostok and Zenit-2 authorised. Nation: USSR. Spacecraft: Vostok, Zenit-2, Zenit-4, Zenit. Central Committee of the Communist Party and Council of Soviet Ministers Decree 569-264 'On work on a reconnaissance satellite and piloted spaceship' was issued. Due to a bitter fight with the military over the nature and priority of the manned spacecraft and photo-reconnaissance space programs, the final decree for the Vostok manned spacecraft was delayed until seven months after drawing release began. This authorised production of a single design that could be used either as a manned spacecraft or as a military reconnaissance satellite. These were the Zenit-2 and Zenit-4 spacecraft based on the Vostok design. This marked the end of the original Zenit configuration. The military had to develop the recovery forces and techniques for both spacecraft, including appropriate aircraft, helicopters, and handling equipment. At that time it was felt that there was a 60% chance on each launch of an abort requiring rescue operations for the cosmonaut.
References: 474.
1959 May 22 - -
The Project Mercury balloon flight test program was canceled. Nation: USA. Program: Mercury. Spacecraft: Mercury. The Space Task Group oficials determined that the spacecraft could be tested environmentally in the Lewis Research Center's altitude wind tunnel. This included correct temperature and altitude simulations to 80,000 feet. The pilot could exercise the attitude control system and retrorockets could be fired in the tunnel. Because an active contract did exist with the Air Force, it was decided the two balloon drop tests with unmanned boiler-plate spacecraft would be accomplished.
References: 483.
1959 May 22 - -
Vostok / Zenit-3 decree issued. Nation: USSR. Spacecraft: Vostok, Zenit-2, Zenit-4, Zenit. Due to a bitter fight with the military over the nature and priority of the manned spacecraft and photo-reconnaissance space programs, the final decree for the Vostok manned spacecraft was delayed until seven months after drawing release began. This authorised production of a single design that could be used either as a manned spacecraft or as a military reconnaissance satellite. These were the Zenit-2 and Zenit-4 spacecraft based on the Vostok design. This marked the end of the original Zenit configuration.
1959 May 23 - 02:42 GMT - Launch Site: Cape Canaveral. Launch Complex: LC18B. Launch Pad: LC18B. Launch Vehicle: Delta. Model: Thor DM-18A. LV Configuration: Thor DM-18A 184. -
Series IV research and development launch Nation: USA. Agency: USAF. Apogee: 520 km (320 mi). References: 2.
1959 May 25-26 - Launch Vehicle: Nova, Saturn C-2, Saturn C-3, Saturn V. -
National booster program, Dyna-Soar, and Mercury discussed Nation: USA. Program: Apollo. Spacecraft: Mercury. The national booster program, Dyna-Soar, and Project Mercury were discussed by the Research Steering Committee. Members also presented reviews of Center programs related to manned space flight. Maxime A. Faget of STG endorsed lunar exploration as the present goal of the Committee although recognizing the end objective as manned interplanetary travel. George M. Low of NASA Headquarters recommended that the Committee: - Adopt the lunar landing mission as its long-range objective.
- Investigate vehicle staging so that Saturn could be used for manned lunar landings without complete reliance on Nova.
- Make a study of whether parachute or airport landing techniques should be emphasized.
- Consider nuclear rocket propulsion possibilities for space flight.
- Attach importance to research on auxiliary power plants such as hydrogen-oxygen systems.
References: 16.
1959 May 25-26 - -
Tentative manned space flight priorities Nation: USA. Program: Apollo. Spacecraft: Mercury. Tentative manned space flight priorities were established by the Research Steering Committee: Project Mercury, ballistic probes, environmental satellite, maneuverable manned satellite, manned space flight laboratory, lunar reconnaissance satellite, lunar landing, Mars Venus reconnaissance, and Mars-Venus landing. The Committee agreed that each NASA Center should study a manned lunar landing and return mission, the study to include the type of propulsion, vehicle configuration, structure, anti guidance requirements. Such a mission was an end objective; it did not have to be supported on the basis that it would lead to a more useful end. It would also focus attention at the Centers on the problems of true space flight.
References: 16.
1959 May 26 - Launch Vehicle: Saturn I. -
First H-1 engine for Saturn I fired. Nation: USA. Program: Apollo. ABMA static fired a single H-1 Saturn engine at Redstone Arsenal, Ala. References: 17, 27.
1959 May 27 - -
STG staff discusses the possibility of an advanced manned spacecraft Nation: USA. Program: Apollo. Director Robert R. Gilruth met with members of his STG staff (Paul E. Purser, Charles J. Donlan, James A. Chamberlin, Raymond L. Zavasky, W. Kemble Johnson, Charles W. Mathews, Maxime A. Faget, and Charles H. Zimmeman) and George M. Low from NASA Headquarters to discuss the possibility of an advanced manned spacecraft.
References: 16.
1959 May 27 - 04:51 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun AA6.161C. -
Aeronomy mission Nation: USA. Agency: USAF. Apogee: 169 km (105 mi). References: 2.
1959 May 27 - 19:55 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun AA6.162C. -
Aeronomy mission Nation: USA. Agency: USAF. Apogee: 177 km (109 mi). References: 2.
1959 May 28 - Launch Vehicle: Little Joe. -
First two Mercury Little Joe booster airframes delivered Nation: USA. Program: Mercury. North American Aviation delivered the first two Little Joe booster airframes, and noted that the four remaining were on fabrication schedule. The planned program was moving smoothly, for rocket motors to be used in the first flight were available at Wallops Station, Virginia, the test flight launching site. In addition, procurement of the test spacecraft incorporating Mercury flight items was on schedule, and the first spacecraft had been instrumented by Space Task Group personnel. Work was also in progress on other test spacecraft.
References: 483.
1959 May 28 - -
A quick-release, side exit hatch was designed for the Mercury spacecraft. Nation: USA. Program: Mercury. Spacecraft: Mercury. The design consisted of a continuous double explosive train to assure that all bolts were actually broken upon activation of the device. References: 483.
1959 May 28 - 07:35 GMT - Launch Site: Cape Canaveral. Launch Complex: LC26B. Launch Pad: -. Launch Vehicle: Jupiter. LV Configuration: Jupiter IRBM AM-18. -
Bioflight 2 Test/Ionosphere mission Nation: USA. Agency: USAF/ABMA. Apogee: 483 km (300 mi). Able and Baker recovered after spaceflight. Fired from AMR at 0235 hours EST. The flight was successful with impact ranging from 0.1 to 0.4 nm from the target. The missile travelled a 1,302 nm range. The significant mission of the missile was to test the effects of cosmic radiation, increased gravity, and weightlessness on live passengers and biomedical experiments of material housed in the nose cone. On board were an American-born rhesus monkey, Able; a squirrel monkey, Baker; and the biomedical experiments -- yeast , corn, mustard seeds, fruit-fly larvae, human blood, mould spore, and fish eggs. Able and Baker were recovered unharmed within one and one-half hours after lift-off. This milestone marked the first recovery of living creatures from a flight through near space. The biomedical experiments were for NASA analysis. Telemetry data disclosed that the responses of the animals were normal for the conditions they were experiencing. During the boost phase, when the higher g-loads were being sustained, body temperature, respiration, pulse rate, and heartbeat rose but were well within tolerable limits. During the weightless period along the trajectory arc, the physiological responses of Able and Baker approached normal - so near, in fact, that according to telemetry data, Baker appeared either to doze or to become drowsy. Upon reentry, the responses rose again, but at landing the animals were nearing a settled physiological state. This flight was another milestone proving that life could be sustained in a space environment.
References: 2.
1959 May 30 - 21:42 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7. LV Configuration: R-7 No. IZ-22. FAILURE: Failure. -
GCh No. IZ-22 (III) test Nation: USSR. Agency: MVS. Apogee: 1,000 km (600 mi). Landed far from aim point. References: 2.
1959 June 1 - Launch Vehicle: Titan. -
Dyna-Soar contractors Boeing and Martin selected. Nation: USA. Spacecraft: Dynasoar. The Dyna-Soar source selection board completed its evaluation of the proposals of the Boeing Airplane Company and the Martin Company. The board recommended the development of the Boeing glider but also favored the employment of the orbtal Titan C booster offered by Martin.
1959 June 1 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-13. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 150 km (90 mi). References: 2.
1959 June - -
Recoverable Interplanetary Space Probe study Nation: USA. Program: Apollo. Spacecraft: RISP. A report entitled "Recoverable Interplanetary Space Probe" was issued at the direction of C. Stark Draper, Director of the Instrumentation Laboratory, MIT. Several organizations had participated in this study, which began in 1957. References: 16.
1959 June - -
Northrop to fabricate the landing system for Mercury. Nation: USA. Program: Mercury. Spacecraft: Mercury. McDonnell selected Northrop as the subcontractor to design and fabricate the landing system for Project Mercury. Northrop technology for landing and recovery systems dated back to 1943 when that company developed the first parachute recovery system for pilotless aircraft. For Project Mercury, Northrop developed the 63-foot ring-sail main parachute.
References: 483.
1959 June - Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 2D. -
Atlas 2D blows up. Nation: USA. Missile 2D blows up on Sycamore stand S-2, after a total of 1486 seconds running time References: 4460.
1959 June 3 - Launch Vehicle: Saturn I. -
Construction begins of the first Saturn launch complex Nation: USA. Program: Apollo. Construction of the first Saturn launch area, Complex 34, began at Cape Canaveral, FIa. References: 16.
1959 June 3 - 20:09 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena A. LV Configuration: Thor Agena A 174 / Agena A 1020. FAILURE: No telemetry after Agena ignition. -
Discoverer 3 Nation: USA. Payload: KH-1 prototype / Agena A 1018. Mass: 753 kg (1,660 lb). Class: Surveillance. Type: Military. Spacecraft: KH-1. Agency: DARPA. COSPAR: F590603A. Decay Date: 1959-06-03. KH-1 prototype; did not carry camera; film capsule recovery failed. References: 126.
-
SRV Nation: USA. Spacecraft: KH-1. Agency: USAF. COSPAR: F590603B. References: 279.
1959 June 4 - -
Post-Mercury program using maneuverable Mercury spacecraft Nation: USA. Program: Apollo. Spacecraft: Mercury. At an STG staff meeting, Director Robert R. Gilruth suggested that study should be made of a post-Mercury program in which maneuverable Mercury spacecraft would make land landings in limited areas. References: 16.
1959 June 4 - -
Mercury follow-on program using maneuverable Mercury capsules. Nation: USA. Spacecraft: Mercury Mark I. At a staff meeting, Space Task Group Director Robert R. Gilruth suggested studying a Mercury follow-on program using maneuverable Mercury capsules for land landings in predetermined areas.
1959 June 4 - -
OKB Filial 2 created. Nation: USSR. Decree 191 'On creation of OKB-1 Branch No. 2 at Krasnoyarsk-26 GKOT' was issued. References: 474.
1959 June 4 - Launch Site: AMR DZ. Launch Complex: -. Launch Pad: 29.0 N x 79.0 W. Launch Vehicle: High Virgo. -
High Virgo satellite interceptor mission Nation: USA. Agency: USAF. Apogee: 51 km (31 mi). References: 2.
1959 June 5 - Launch Site: Cape Canaveral. Launch Complex: -. Launch Pad: -. Launch Vehicle: Saturn I. -
Saturn I launch complex construction starts. Nation: USA. Program: Apollo. References: 17, 27.
1959 June 5 - Launch Vehicle: Atlas. Model: Atlas D. -
Flight instrumentation necessary to support the Mercury-Atlas program. Nation: USA. Program: Mercury. Space Technology Laboratories and Convair completed an analysis of flight instrumentation necessary to support the Mercury-Atlas program. The primary objective of the study was to select a light-weight telemetry system. A system weighing 270 pounds was recommended, and the National Aeronautics and Space Administration concurred with the proposal.
References: 483.
1959 June 5 - 04:15 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trailblazer. Model: Trailblazer 1. LV Configuration: Trailblazer 1 TB I beta?. -
Re-entry Vehicle test Nation: USA. Agency: NASA. Apogee: 260 km (160 mi). References: 2.
1959 June 6 - Launch Vehicle: Jupiter. Model: Juno II. -
Jupiter biological test results. Nation: USA. Army announced that sea urchin eggs fertilized before Jupiter nose cone flight continued to grow normally. References: 17.
1959 June 6 - 17:39 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 5D. FAILURE: Failure. -
Research and development launch Nation: USA. Agency: USAF. References: 2.
1959 June 8 - -
Project Horizon Phase I report Nation: USA. Program: Horizon. The Project Horizon Phase I report was completed. In it, a U.S. manned landing on the moon in 1965 was proposed, to be followed in 1966 by an operational lunar outpost. Expenditures would average $667 million a year from Fiscal Year 1960 through Fiscal Year 1968. The guiding philosophy of the report was one of "enlightened conservatism of technical approach." On July 28 the report was presented to the Secretary of the Army and the Chief of Staff.
Additional Details: Project Horizon Phase I report. References: 16.
1959 June 8 - -
Project Horizon report conceived years using a booster's spent stage as a space station's basic structure. Nation: USA. Program: Horizon. Spacecraft: Horizon Station. In a Project Horizon report, Wernher von Braun, then with the Army Ballistic Missile Agency, advanced a theory that he had conceived years earlier for using a booster's spent stage as a space station's basic structure. This later evolved into the 'wet stage' concept for the Skylab Program.
1959 June 8 - -
Mercury Big Joe spacecraft for the reentry test was delivered to Cape Canaveral. Nation: USA. Program: Mercury. References: 483.
1959 June 8 - Launch Site: AMR DZ. Launch Complex: -. Launch Pad: 29.0 N x 79.0 W. Launch Vehicle: Bold Orion. Model: Bold Orion 2. LV Configuration: Bold Orion-1. -
Interceptor mission Nation: USA. Agency: USAF. Apogee: 100 km (60 mi). References: 2.
1959 June 8 - 16:38 GMT - Launch Site: Rosamund Dry Lake DZ. Launch Complex: -. Launch Pad: 34.7 N x 118.1 W. Launch Vehicle: X-15. LV Configuration: X-15 1-1-5. -
X-15A test Nation: USA. Agency: NASA/USAF. Apogee: 11 km (6 mi). First flight for X-15 # 1. Planned glide flight. Maximum Speed - 840 kph. Maximum Altitude - 11445 m. References: 2.
1959 June 9 - 20:34 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7. FAILURE: Failure. -
GCh No. IZ-23 (III) test Nation: USSR. Agency: MVS. Apogee: 1,000 km (600 mi). Landed far from aim point. References: 2.
1959 June 10 - 16:40 GMT - Launch Site: Holloman. Launch Complex: A. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AA3.280C. -
Ionosphere mission Nation: USA. Agency: USAF. Apogee: 225 km (139 mi). References: 2.
1959 June 11 - 06:44 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Able II. LV Configuration: Thor Able II 137. -
RVX-1 Re-entry Vehicle test Nation: USA. Agency: USAF. Apogee: 520 km (320 mi). References: 2.
1959 June 11 - 13:03 GMT - Launch Site: Woomera. Launch Complex: LA5A. Launch Pad: -. Launch Vehicle: Black Knight. Model: Black Knight 201. LV Configuration: Black Knight-201 BK.04. -
Research and development launch Nation: UK. Agency: RAE. Apogee: 803 km (498 mi). References: 2.
1959 June 14-27 - -
Mercury spacecraft being designed to withstand 149 decibels. Nation: USA. Program: Mercury. Spacecraft: Mercury. A visit was made to McDonnell and it was learned that the Mercury spacecraft was being designed structurally to withstand 149 decibels overall noise level. McDonnell, however, anticipated that the actual maximum level would not be above 128 decibels. Space Task Group personnel felt that even the 128 decibels were too high for pilot comfort, and extensive research toward the resolution of this matter was started.
References: 483.
1959 June 16 - 21:45 GMT - Launch Site: Vandenberg. Launch Complex: SLC10E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DM-18A. LV Configuration: Thor DM-18A 191. FAILURE: Autopilot error. -
IWST test flight Nation: USA. Agency: RAF. Apogee: 0 km ( mi). Integrated Weapon System Training Launch 2 References: 2.
1959 June 18 - Launch Vehicle: Saturn I. -
NASA funded study of a lunar exploration program based on Saturn Nation: USA. Program: Apollo. NASA authorized $150,000 for Army Ordnance Missile Command studies of a lunar exploration program based on Saturn-boosted systems. To be included were circumlunar vehicles, unmanned and manned; close lunar orbiters; hard lunar impacts; and soft lunar landings with stationary or roving payloads.
References: 16.
1959 June 18 - -
Centrifuge program to investigate the role of a pilot in the launch of a multi-stage vehicle. Nation: USA. Program: Mercury. A centrifuge program was conducted at Johnsville, Pennsylvania, to investigate the role of a pilot in the launch of a multi-stage vehicle. Test subjects were required to perform boost-control tasks, while being subjected to the proper boost-control accelerations. The highest g-force experienced was 15, and none of the test subjects felt they reached the limit of their control capability. As a note of interest, one of the test subjects, Neil Armstrong, was later selected for the Gemini program in September 1962.
References: 483.
1959 June 18 - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Luna 8K72. LV Configuration: Vostok-L 8K72 I1-7. FAILURE: Inertial system failed at 153 seconds after launch. Vehicle destroyed by range safety. -
Luna failure - inertial system failed at T+153 seconds Nation: USSR. Program: Luna. Payload: E-1A s/n 5. Class: Planetary. Type: Lunar. Spacecraft: Luna E-1A. Agency: MVS. COSPAR: F590618A. References: 175.
1959 June 19 - Launch Site: Cape Canaveral. Launch Complex: -. Launch Pad: -. Launch Vehicle: Bold Orion. Model: Bold Orion 2. LV Configuration: Bold Orion-1. -
Interceptor mission Nation: USA. Agency: USAF. Apogee: 100 km (60 mi). References: 2.
1959 June 20 - Launch Vehicle: DF-2, K-13, Kosmos 2, P-15. -
Decision to withhold R-12 and nuclear warhead drawing package from China over Sidewinder affair Nation: China. Spacecraft: Project 581. The Soviet Central Committee advises China it will not provide prototype or drawings of atomic bombs as agreed previously. Khrushchev promised China that he would provide the drawing package for the R-12 IRBM as soon as testing was completed. However then came the affair of the Sidewinder. At the end of 1958 or early 1959 a complete missile fell into the hands of the Chinese. They promised to provide it to the Russians, but then dragged their feet. They were finally told in February 1959 that unless they provided the Sidewinder, they would not be given the R-12 package. The missile was finally delivered but it was found that the key crystal in the infrared homing sensor was missing. The Chinese had also been caught disassembling a P-15 cruise missile at a training facility in China. It had taken the Russian trainers two days to get it reassembled correctly. Therefore on June 20 1959 the decision was taken not to transfer the R-12 or the promised nuclear warhead design to China.
The Soviets created a new design bureau to copy the Sidewinder. Fabrication of the crystal for the infrared sensor was the main obstacle. The initial production batches had a 99% rejection rate. A state commission was set up to get to the bottom of the problem, but couldn’t find a solution. The main problem seemed to be low-quality ore provided by the mines.
References: 87.
1959 June 21 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5V. -
Solar x-ray mission Nation: USSR. Agency: AN SSSR. Apogee: 400 km (240 mi). References: 2.
1959 Summer - -
STG worked on advanced design concepts of earth orbital and lunar missions Nation: USA. Program: Apollo. Spacecraft: Mercury. Members of STG - including H. Kurt Strass, Robert L. O'Neal, Lawrence W. Enderson, Jr., and David C. Grana - and Thomas E. Dolan of Chance Vought Corporation worked on advanced design concepts of earth orbital and lunar missions. The goal was a manned lunar landing within ten years, rather than an advanced Mercury program.
References: 16.
1959 June 22 - -
Preliminary design of a two-man space laboratory. Nation: USA. Program: Gemini. Spacecraft: Gemini, MOL. H. Kurt Strass of Space Task Group's Flight Systems Division (FSD) recommended the establishment of a committee to consider the preliminary design of a two-man space laboratory. Representatives from each of the specialist groups within FSD would work with a special projects group, the work to culminate in a set of design specifications for the two-man Mercury.
1959 June 22 - Launch Site: Kapustin Yar. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-2. Model: R-2A. -
R-2A launch Nation: USSR. Agency: NII-88. Apogee: 212 km (131 mi). References: 2, 283.
1959 June 22 - 14:32 GMT - Launch Site: Holloman. Launch Complex: A. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee. LV Configuration: Aerobee AA1.260C. -
Solar infrared mission Nation: USA. Agency: USAF. Apogee: 110 km (60 mi). References: 2.
1959 June 22 - 20:16 GMT - Launch Site: Cape Canaveral. Launch Complex: LC18A. Launch Pad: LC18A. Launch Vehicle: Vanguard. Model: Vanguard. LV Configuration: Vanguard SLV-6. FAILURE: Stage 2 propulsion malfunction. -
Vanguard 3B Nation: USA. Program: Vanguard. Payload: Radiation Balance satellite. Mass: 10 kg (22 lb). Class: Earth. Type: Magnetosphere. Spacecraft: Vanguard 3. Agency: NASA. Apogee: 140 km (80 mi). COSPAR: F590622A. Decay Date: 1959-06-22. References: 126.
1959 June 24 - Launch Vehicle: Redstone. Model: Redstone MRLV. -
Eight Mercury Redstone launch vehicles final cost $20.1 million. Nation: USA. Program: Mercury. Against an original estimated cost of $15.5 million for eight Redstone launch vehicles in support of Project Mercury, the final negotiated figure was $20.1 million. References: 483.
1959 June 24 - 12:10 GMT - Launch Site: Holloman. Launch Complex: A. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AA3.220C. -
Ionosphere mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1959 June 25 - -
Mercury recovery airdrop test. Nation: USA. Program: Mercury. Spacecraft: Mercury. Navy surface vessels and aircraft were used in a recovery operation after an airdrop of a spacecraft off the coast from Jacksonville, Florida. The spacecraft was purposely dropped 40 miles away from the predicted impact point and 45 miles away from the nearest ship. Recovery was effected in 2 and one half hours.
References: 483.
1959 June 25-26 - -
Steps toward a manned lunar landing Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. At the second meeting of the Research Steering Committee on Manned Space Flight, held at the Ames Research Center, members presented reports on intermediate steps toward a manned lunar landing and return.Bruce T. Lundin of the Lewis Research Center reported to members on propulsion requirements for various modes of manned lunar landing missions, assuming a 10,000-pound spacecraft to be returned to earth. Lewis mission studies had shown that a launch into lunar orbit would require less energy than a direct approach and would be more desirable for guidance, landing reliability, etc. From a 500,000 foot orbit around the moon, the spacecraft would descend in free fall, applying a constant-thrust decelerating impulse at the last moment before landing. Research would be needed to develop the variable-thrust rocket engine to be used in the descent. With the use of liquid hydrogen, the launch weight of the lunar rocket and spacecraft would be 10 to 11 million pounds.
Additional Details: Steps toward a manned lunar landing. References: 16.
1959 June 25-26 - Launch Vehicle: Saturn C-2. -
Lunar mission studies under way at the Army Nation: USA. Program: Horizon. Spacecraft: Mercury. During the Research Steering Committee meeting, John H. Disher of NASA Headquarters discussed the lunar mission studies under way at the Army Ballistic Missile Agency (ABMA). Additional Details: Lunar mission studies under way at the Army. References: 16.
1959 June 25-26 - -
Projected manned space station Nation: USA. Program: Apollo. A report on a projected manned space station was made to the Research Steering Committee by Laurence K. Loftin, Jr., of the Langley Research Center. In discussion, Chairman Harry J. Goett expressed his opinion that consideration of a space laboratory ought to be an integral and coordinated part of the planning for the lunar landing mission. George M. Low of NASA Headquarters warned that care should be exercised to assure that each step taken toward the goal of a lunar landing was significant, since the number of steps that could be funded was extremely limited.
References: 16.
1959 June 25-26 - -
Research Steering Committee briefed on technical studies Nation: USA. Program: Apollo. Spacecraft: Mercury. Alfred J. Eggers, Jr., of the Ames Research Center told the members of the Research Steering Committee of studies on radiation belts, graze and orbit maneuvers on reentry, heat transfer, structural concepts and requirements, lift over drag considerations, and guidance systems which affected various aspects of the manned lunar mission. Eggers said that Ames had concentrated on a landing maneuver involving a reentry approach over one of the poles to lessen radiation exposure, a graze through the outer edge of the atmosphere to begin an earth orbit, and finally reentry and landing.
Additional Details: Research Steering Committee briefed on technical studies. References: 16.
1959 June 25-26 - Launch Vehicle: Saturn V. -
Study and research areas for manned flight to and from the moon Nation: USA. Program: Apollo. Spacecraft: Mercury. Members of the Research Steering Committee determined the study and research areas which would require emphasis for manned flight to and from the moon and for intermediate flight steps: Additional Details: Study and research areas for manned flight to and from the moon. References: 16.
1959 June 25-26 - -
Space stations second priority to a lunar landing mission. Nation: USA. Laurence K. Loftin, Jr., of Langley Research Center, presented to the Research Steering Committee on Manned Space Flight a report on a projected manned space station. During subsequent discussion, Committee Chairman Harry J. Goett stated that considerations of space stations and orbiting laboratories should be an integral part of coordinated planning for a lunar landing mission.
Additional Details: Space stations second priority to a lunar landing mission..
1959 June 25 - 22:47 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena A. LV Configuration: Thor Agena A 179 / Agena A 1023. FAILURE: Insufficient stage 2 velocity. -
Discoverer 4 Nation: USA. Payload: KH-1 9001. Mass: 743 kg (1,638 lb). Class: Surveillance. Type: Military. Spacecraft: KH-1. Agency: DARPA. COSPAR: F590625A. Decay Date: 1959-06-25. KH-1; 1st generation low resolution photo surveillance. Failed to achieve orbit. References: 126.
-
SRV 102 Nation: USA. Spacecraft: KH-1. Agency: USAF. COSPAR: F590625B. References: 279.
1959 June 26 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier ASROC Cajun. LV Configuration: Terrier ASROC Cajun Terasca. -
Radar beacon test Nation: USA. Agency: USN. Apogee: 100 km (60 mi). References: 2.
1959 June 26 - Launch Site: Cape Canaveral. Launch Complex: LC18B. Launch Pad: LC18B. Launch Vehicle: Delta. Model: Thor DM-18A. LV Configuration: Thor DM-18A 198. -
Series IV research and development launch Nation: USA. Agency: USAF. Apogee: 520 km (320 mi). References: 2.
1959 June 28 - Launch Vehicle: Little Joe. -
Ablation materials for the Mercury Little Joe flights. Nation: USA. Program: Mercury. Spacecraft: Mercury. Between June 28 and July 11, 1959, 12 heat-transfer tests were made in the Preflight Jet Test facility at Wallops Island on several ablation materials being considered for use on the spacecraft afterbody (not heat shield) for the Little Joe flights. Test conditions simulated those of actual Little Joe trajectories. Of the materials used, triester polymer and thermolag demonstrated the capability to protect the spacecraft against expected heat loads.
References: 483.
1959 June 29 - Launch Site: Aberporth. Launch Complex: -. Launch Pad: -. Launch Vehicle: Rook. FAILURE: Failure. -
Test mission Nation: UK. Agency: RAE. Apogee: 0 km ( mi). References: 2.
1959 June 29 - 11:33 GMT - Launch Site: Woomera. Launch Complex: LA5A. Launch Pad: -. Launch Vehicle: Black Knight. Model: Black Knight 201. LV Configuration: Black Knight-201 BK.05. -
Research and development launch Nation: UK. Agency: RAE. Apogee: 442 km (274 mi). References: 2.
1959 June 29 - 15:42 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris AX. LV Configuration: Polaris AX-9. -
Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1959 June 30 - 02:37 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DM-18A. LV Configuration: Thor DM-18A 194. -
Series IV Lofted Trajectory research and development mission Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi). References: 2.
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