Flight test performance and description of a rocket vihicle for producing low-speed artificial meteors

Flight test performance and description of a rocket vehicle for producing low-speed artificial meteors /

Brown, Clarence A.
Keating, Jean C.
Langley Research Center.

Prepared at Langley Research Center."April 1964"--Cover.Includes bibliographical references (p. 9).M...

Meteoroid Physics Research at MSFC Reviews, Mar. 1968 - Mar. 1970

January 1969

Photographic and visual observation of meteoroid density and simulation of hypervelocity impact usin...

A study to define a state-of-the-art rocket vehicle suitable for synoptic meteorological soundings, volume 1 Final report

June 1965

Rocket vehicle for synoptic meteorological soundings - evaluation of four proposed system

Luminous efficiency of an artificial meteor at 11.9 kilometers per second

Ayers, W. G.

August 1965

Trailblazer II reentry vehicle artificial meteoroid experiment consisting of reentering 2.2-gram st...

Luminous efficiencies of three nickel artificial meteors between 9.8 and 11.4 kilometers per second

Bess, T. D.

August 1968

Luminous intensity and efficiency parameters for hypersonic reentry of nickel artificial meteor

PERFORMANCE AND SOME DESIGN ASPECTS OF THE FOUR-STAGE SOLIDPROPELLANT ROCKET VEHICLE USED IN THE RAM A1 FLIGHT TEST

Levine, J.

March 1963

Radio-attenuation measurement /ram a1/ test, four- stage solid-propellant rocket vehicle - performan...

Flight Investigation of the Performance of a Two-stage Solid-propellant Nike-deacon (DAN) Meteorological Sounding Rocket

Heitkotter, Robert H

July 1956

A flight investigation of two Nike-Deacon (DAN) two-stage solid-propellant rocket vehicles indicated...

Ionization probability of iron particles at meteoritic velocities

Friichtenicht, J. F.
Slattery, J. C.

February 1966

Ion production for ablation of micron size iron particles moving at supersonic speed in air and argo

A study of artificial meteors as ablators

Stine, H. A.
Shepard, C. E.
Winovich, W.
Vorreiter, J. W.

January 1965

Ablation properties and luminosity of artificial meteoroid materials determined in plasma jet test

Aerodynamic characteristics of two trailblazer ii blunted 9 deg cone reentry bodies at mach 6.8 in air and 21.2 in helium

Schippell, H. R.
Neal, L., Jr.
Marcum, D. C., Jr.

May 1965

Effect of aerodynamic characteristics of nose bluntness on electromagnetic and luminous efficiency b...

Balloon launched decelerator test program: Post-test test report

Dickinson, D.
Schlemmer, J.
Michel, F.
Hicks, F.
Moog, R. D.

September 1972

Balloon Launched Decelerator Test (BLDT) flights were conducted during the summer of 1972 over the W...

Development of meteoroid simulators for hypervelocity impact studies

Woodall, R. L.
Berus, E. R.

October 1970

Developing aluminum meteoritic simulators for hypervelocity impact test using shaped charge

Description of the meteoroid detection experiment flown on the Pioneer 10 and 11 Jupiter flyby missions

Oneal, R. L.

August 1974

The meteoroid detection experiment has the objective of measuring the population of 10 to the minus ...

A Five-Stage Solid-Fuel Sounding-Rocket System

Swanson, Andrew G.

March 1959

A five-stage solid-fuel sounding-rocket system which can boost a payload of 25 pounds to an altitude...

Small iron meteoroids

David Čapek
Pavel Koten
Jiří Borovička
Vlastimil Vojáček
Pavel Spurný
Rostislav Štork

May 2019

Context. A significant fraction of small meteors are produced by iron meteoroids. Their origin and t...

Flight test performance and description of a rocket vehicle for producing low-speed artificial meteors /

Brown, Clarence A.
Keating, Jean C.
Langley Research Center.

Prepared at Langley Research Center."April 1964"--Cover.Includes bibliographical references (p. 9).M...

Meteoroid Physics Research at MSFC Reviews, Mar. 1968 - Mar. 1970

January 1969

Photographic and visual observation of meteoroid density and simulation of hypervelocity impact usin...

A study to define a state-of-the-art rocket vehicle suitable for synoptic meteorological soundings, volume 1 Final report

June 1965

Rocket vehicle for synoptic meteorological soundings - evaluation of four proposed system

Luminous efficiency of an artificial meteor at 11.9 kilometers per second

Ayers, W. G.

August 1965

Trailblazer II reentry vehicle artificial meteoroid experiment consisting of reentering 2.2-gram st...

Luminous efficiencies of three nickel artificial meteors between 9.8 and 11.4 kilometers per second

Bess, T. D.

August 1968

Luminous intensity and efficiency parameters for hypersonic reentry of nickel artificial meteor

PERFORMANCE AND SOME DESIGN ASPECTS OF THE FOUR-STAGE SOLIDPROPELLANT ROCKET VEHICLE USED IN THE RAM A1 FLIGHT TEST

Levine, J.

March 1963

Radio-attenuation measurement /ram a1/ test, four- stage solid-propellant rocket vehicle - performan...

Flight Investigation of the Performance of a Two-stage Solid-propellant Nike-deacon (DAN) Meteorological Sounding Rocket

Heitkotter, Robert H

July 1956

A flight investigation of two Nike-Deacon (DAN) two-stage solid-propellant rocket vehicles indicated...

Ionization probability of iron particles at meteoritic velocities

Friichtenicht, J. F.
Slattery, J. C.

February 1966

Ion production for ablation of micron size iron particles moving at supersonic speed in air and argo

A study of artificial meteors as ablators

Stine, H. A.
Shepard, C. E.
Winovich, W.
Vorreiter, J. W.

January 1965

Ablation properties and luminosity of artificial meteoroid materials determined in plasma jet test

Aerodynamic characteristics of two trailblazer ii blunted 9 deg cone reentry bodies at mach 6.8 in air and 21.2 in helium

Schippell, H. R.
Neal, L., Jr.
Marcum, D. C., Jr.

May 1965

Effect of aerodynamic characteristics of nose bluntness on electromagnetic and luminous efficiency b...

Balloon launched decelerator test program: Post-test test report

Dickinson, D.
Schlemmer, J.
Michel, F.
Hicks, F.
Moog, R. D.

September 1972

Balloon Launched Decelerator Test (BLDT) flights were conducted during the summer of 1972 over the W...

Development of meteoroid simulators for hypervelocity impact studies

Woodall, R. L.
Berus, E. R.

October 1970

Developing aluminum meteoritic simulators for hypervelocity impact test using shaped charge

Description of the meteoroid detection experiment flown on the Pioneer 10 and 11 Jupiter flyby missions

Oneal, R. L.

August 1974

The meteoroid detection experiment has the objective of measuring the population of 10 to the minus ...

A Five-Stage Solid-Fuel Sounding-Rocket System

Swanson, Andrew G.

March 1959

A five-stage solid-fuel sounding-rocket system which can boost a payload of 25 pounds to an altitude...

Small iron meteoroids

David Čapek
Pavel Koten
Jiří Borovička
Vlastimil Vojáček
Pavel Spurný
Rostislav Štork

May 2019

Context. A significant fraction of small meteors are produced by iron meteoroids. Their origin and t...

Flight test performance and description of a rocket vehicle for producing low-speed artificial meteors /

Brown, Clarence A.
Keating, Jean C.
Langley Research Center.

Prepared at Langley Research Center."April 1964"--Cover.Includes bibliographical references (p. 9).M...

Meteoroid Physics Research at MSFC Reviews, Mar. 1968 - Mar. 1970

January 1969

Photographic and visual observation of meteoroid density and simulation of hypervelocity impact usin...

A study to define a state-of-the-art rocket vehicle suitable for synoptic meteorological soundings, volume 1 Final report

June 1965

Rocket vehicle for synoptic meteorological soundings - evaluation of four proposed system

Flight test performance and description of a rocket vihicle for producing low-speed artificial meteors

Abstract

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Flight test performance and description of a rocket vihicle for producing low-speed artificial meteors

Abstract

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