| astronautix.com | Chronology - 1957 - Quarter 3 |
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- 1957 Jul 1 - Nation: USA. Launch Vehicle: Aerobee.
Aerobee upper air research rocket developed by the Applied Physics Laboratory of Johns Hopkins, and first fired on September 25, 1947, completed 165 successful firings to date. References: 17 .
- 1957 July - Nation: USA. Launch Vehicle: Scout A.
A study was initiated by the Langley Aeronautical Laboratory on the use of solid-fuel upper stages to achieve a payload orbit with as simple a launch vehicle as possible. This was the beginning of the Scout test-vehicle concept. References: 483 .
- 1957 Jul 1 - Nation: USA. Launch Site: Vandenberg . Launch Vehicle: Atlas D.
Air Research and Development Command activated the 704th Strategic Missile Wing (Atlas) at Cooke AFB. References: 88 , 278 .
These included development of a three stage version of R-7, development of satellite guidance and control systems of the precision required for photography from orbit, satellite control equipment, ELINT sensors, guidance systems, film cassette return systems, and tracking systems for recovery of the re-entry vehicle with the film cassette.
- 1957 Jul 11 - Nation: USA. Launch Vehicle: Navaho G-26.
Navaho ramjet intercontinental missile program canceled by Air Force. References: 17 .
- 1957 Jul 11 - Nation: USA.
NACA flight 10. Aborted after launch, indication of open landing-gear door. Propellants jettisoned, completed as a glide flight. References: 49 , 97 .
- 1957 Jul 12 - Nation: USSR. Launch Site: Kapustin Yar . Launch Vehicle: R-12.
- 1957 Jul 12 - Nation: USA.
- 1957 Jul 12 - - 06:30 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC6. Launch Vehicle: Jupiter A. LV Configuration: Redstone s/n CC-35. FAILURE: Control system malfunction at re-entry.
Launched at 0130 hours EST from AMR. The primary test objective was to test the accuracy of the guidance system. The flight was successful. Actual range was 130.125 nm; 0.15 nm over; and 285 meters left of the intended impact point. All missions were successfully accomplished. The missile followed the predicted trajectory very closely. Survey of the impact crater indicated a miss distance of 50 meters over and 284 meters to the left of the predicted impact point, giving a radial miss distance of 389.5 meters. Missed aimpoint by 289 m. References: 439 .
- 1957 Jul 12 - Nation: USSR. Launch Site: Baikonur . Launch Vehicle: R-7 8K71. LV Configuration: R-7 8K71 M1-7. FAILURE: Failure of the control system due to a short circuit of the battery. Rapid roll developed, resulting in all four strap-on boosters flying away from the core at 33 seconds in the flight.
- 1957 Jul 13 - Nation: USA. Launch Vehicle: Navaho G-26, Navaho G-38.
The supersonic intercontinental cruise missile was made obsolete by the Atlas ICBM. Already-built Navaho G-26 test missiles were flown to the end of 1958. At the time the program was cancelled full-range G-38 missiles were in fabrication with first flight test planned by the end of 1958. The engines, missile frame manufacturing techniques, inertial and stellar navigation equipment, and telemetry/guidance techniques developed for Navaho established the technical basis for all subsequent US rocket developments.
- 1957 Jul 19 - Nation: USA.
NACA flight 11. Mach 1.65 at 18,300 m. Control pulses, sideslips, and 2 g wind-up turn. References: 49 , 97 .
- 1957 Jul 25 - Nation: USA.
- 1957 Jul 25 - - 04:17 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC6. Launch Vehicle: Jupiter A. LV Configuration: Redstone s/n CC-37.
Launched at 2317 hours EST from AMR. The flight was successful. Actual range was 126.227 nm; 147 meters under; and 182 meters left of the intended impact point. The primary test objective was to flight test warhead and fuse functioning as a system. A survey of the warhead impact point: indicated a miss distance of 147 meters short, 182 meters to the left of the predicted impact point, or a radial miss distance of 234 meters. Missed aimpoint by 235 m. References: 439 .
- 1957 Jul 29 - Nation: USA.
NACA flight 12. Enlarged wing tips installed to simulate wing tips to be used with reaction controls. Mach 1.55 at 18,300 m. References: 49 , 97 .
- 1957 Aug 1 - Nation: USA. Launch Vehicle: Atlas D.
Estimated operational capability date for Atlas changed from March 1959 to June 1959. References: 17 , 278 .
- 1957 Aug 1 - Nation: USSR. Launch Site: Kapustin Yar . Launch Vehicle: Burya. LV Configuration: Burya s/n 2/1.
Objective was limited to test of operation of first stage boosters. The AVD Engine Cutoff System activated on ignition due to destruction of an OT-155 propellant valve in one of the booster engines. The missile remained on the pad. The stage boosters were dismounted, checked, and reassembled.
- 1957 Aug 1 - Nation: USA. Launch Site: Cape Canaveral . Launch Vehicle: Thor. LV Configuration: Thor 104. FAILURE: Broke up after 92 seconds.
- 1957 Aug 5 - Nation: Russia.
- 1957 Aug 7 - Nation: USA. Launch Vehicle: Jupiter C.
A Jupiter-C (test vehicle in the Jupiter missile development program), with a scale-model nose cone, was fired 1,200 miles down the Atlantic Missile Range. The nose cone, an ablative type, reached a peak altitude of over 600 miles, and its recovery was one of the proving steps of the ablative reentry principle. The nose cone was displayed by President Eisenhower to a nation-wide television audience on November 7, 1957. References: 483 .
- 1957 Aug 8 - - 06:59 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC6. Launch Vehicle: Jupiter C. LV Configuration: Redstone s/n CC-40.
First Nose Cone Recovery. Army-JPL Jupiter-C fired a scale-model nose cone 1,200 miles down range from AMR with a summit altitude of 600 miles. Recovery the next day of aerodynamic nose cone using ablation, resolved reentry heating problem for Jupiter missile. Nose cone was shown to the Nation on TV by President Eisenhower on November 7.
Fired from AMR at 0159 hours EST, impacted at the predicted range. This success proved conclusively that the planned ablative-type heat protection for Jupiter warheads was satisfactory. The missile was a three-stage configuration--the first stage an elongated Redstone missile, the second and third stages 11 and 3 six-inch scaled Sergeant rockets, respectively. The one-third scale Jupiter nose cone was attached to the final stage with scheme for separation provided. The nose cone travelled to a 1,168 nm range, reached a velocity of 4,004 m/sec, and experienced a total heat input at stagnation point at 95% of that for the full scale nose cone at 1,500 nm. Naval units recovered the scaled nose cone according to plan. References: 439 .
- 1957 Aug 8 - Nation: USA.
NACA flight 13. Stability and control investigation. Mach 1.5 at 18300 m, accelerated maneuvers, control pulses, and pull-ups. References: 49 , 97 .
- 1957 Aug 10 - Nation: USA.
In the summer of 1957 physicist Bob Brownlee attempted to 'contain' the blast effects of an atomic explosion from a device placed at the bottom of a 500 foot vertical shaft in the Nevada desert. A four-inch-thick steel plate weighing 'several hundred pounds' is placed over the hole (diameter not specified). This blew off as expected in the blast and was seen in films to depart the area at six times escape velocity . Brownlee never publicly challenged the Soviet's claim (to having launched the 1st Earth satellite. References: 92 .
- 1957 Aug 15 - Nation: USA.
NACA flight 14. Pilot check. Nose landing gear failed on landing, minor damage. References: 49 , 97 .
- 1957 Aug 19 - Nation: USA.
Manhigh II reached a record altitude of 101,516 feet (30,950 m) with Major David Simons aboard on 19 and 20 August. Including the pilot and scientific equipment, the total weight of the Manhigh II gondola was 747 kg. At maximum altitude, the ballon expanded to a diameter of 60 m with a volume in excess of 85,000 cubic m.
- 1957 Aug 20 - Nation: USSR. Launch Vehicle: R-12.
Ministry of Armaments Decree 'On transfer of two R-12 missiles to China (on August 6)' was issued. References: 474 .
- 1957 Aug 21 - Nation: USSR. Launch Site: Baikonur . Launch Vehicle: R-7 8K71. LV Configuration: R-7 8K71 M1-8.
First successful ICBM flight. Problems with the curing of the nose cone material, known before launch, led to the dummy warhead disintegrating over the Kamchatka Peninsula. References: 98 , 177 .
- 1957 Aug 25 - Nation: USSR. Launch Vehicle: R-2.
- 1957 Aug 26 - Nation: USSR. Launch Site: Baikonur . Launch Vehicle: R-7 8K71.
Soviet Union announces successful launch of a "super longdistance intercontinental multistage ballistic rocket ...a few days ago," according to Tass Soviet News Agency. References: 17 .
- 1957 Aug 28 - Nation: USA. Launch Site: Cape Canaveral . Launch Vehicle: Jupiter. LV Configuration: Jupiter s/n AM-2.
The fourth Jupiter was fired from AMR at 1602 hours EST over IRBM range and was the second successful flight of the series. The range error was 27.5 nm with a 36.5 nm lateral error. Range was predicted for 146 nm. LOX was cut off at 170 seconds. All flight missions were fulfilled satisfactorily. Separation occurred 5 seconds after burnout, as programmed, This was the first test of separation of body from thrust unit. References: 439 .
- 1957 Aug 31 - Nation: USSR. Launch Vehicle: R-2.
- 1957 Sep 1 - Nation: USSR. Launch Site: Kapustin Yar . Launch Vehicle: Burya. LV Configuration: Burya s/n 2/1.
Objective was limited to test of operation of first stage boosters. After launch, there was a premature release of the jet vanes. The missile cleared the launch tower, then immediately arced over and crashed with a huge explosion within sight of the launch pad.
- 1957 Sep 7 - Nation: USSR. Launch Site: Baikonur . Launch Vehicle: R-7 8K71. LV Configuration: R-7 8K71 M1-9.
- 1957 Sep 9 - Nation: USA. Launch Vehicle: Redstone.
The 40th Field Artillery Missile Group, the first heavy missile group organized in the U.S. Army, was transferred from Fort Carson, Colorado, to Redstone Arsenal.
- 1957 Sep 9 - Nation: USA.
- 1957 Sep 9 - Nation: USSR. Launch Vehicle: R-2.
- 1957 Sep 10 - - 02:41 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC6. Launch Vehicle: Jupiter A. LV Configuration: Redstone s/n CC-38. FAILURE: ST-80 pitch program malfunction.
Launched at: 2141 hours EST from AMR. The flight was unsuccessful, The missile impacted 14 77 nm from the launch pad. Mechanical failure of the guidance tilt program caused the missile to assume a very steep trajectory which resulted La. a short range flight. Missed aimpoint by 111,000 m. References: 439 .
- 1957 Sep 15 - Nation: USSR. Launch Site: Kapustin Yar . Launch Vehicle: R-12.
- 1957 Sep 17 - Nation: USA. Launch Site: White Sands . Launch Vehicle: Aerobee. LV Configuration: RTV-N-10.
Solar spectrum research. Launched at 0704 local time. Reached 51.1 km.
- 1957 Sep 19 - Nation: USA.
- 1957 Sep 19 - Nation: USA.
NACA flight 16. Planned mach number not attained, loss of power during pushover from climb. References: 49 , 97 .
- 1957 Sep 20 - Nation: USA. Launch Site: Cape Canaveral . Launch Vehicle: Thor. LV Configuration: Thor 105.
Complete USAF Thor IRBM first successfully launched from Cape Canaveral. Dummy Warhead sent to 1800 km range.
- 1957 Sep 25 - Nation: USA. Launch Vehicle: Atlas A. LV Configuration: Atlas 6A.
Atlas was again destroyed by command signal at three minutes into flight following a failure in the booster fuel system. References: 48 , 278 .
- 1957 Sep 26 - Nation: USA. Launch Vehicle: Rockoon.
Thirty-six Rockoons (balloon-launched rockets) were launched from Navy icebreaker, U.S.S. Glacier, in Atlantic, Pacific, and Antartic areas ranging from 75 N. to 72 S. latitude, as part of the U.S.-IGY scientific program headed by James A. Van Allen and Lawrence J. Cahill of the State University of Iowa (SUI). These were the first known upper atmosphere rocket soundings in the Antartctic area. References: 17 .
- 1957 Sep 30 - Nation: USA.
Scientists from 12 countries, including the United States and U.S.S.R., attended International Rocket and Satellite Conference held at the National Academy of Sciences, Washington, D.C., under the sponsorship of CSAGI. References: 17 .
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