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Refinado por: data de publicação: 1959Até1974 remover
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1
Digital simulation of an aerospace vehicle (Aerospace Vehicle Simulation /AVS/ Program simulating continuous and discrete dynamics of aerospace vehicles and ground support equipment on digital computer)
Digital simulation of an aerospace vehicle (Aerospace Vehicle Simulation /AVS/ Program simulating continuous and discrete dynamics of aerospace vehicles and ground support equipment on digital computer)
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Digital simulation of an aerospace vehicle (Aerospace Vehicle Simulation /AVS/ Program simulating continuous and discrete dynamics of aerospace vehicles and ground support equipment on digital computer)

Mitchell, J R ; Moore, J W ; TRAUBOTH, H H

Digital simulation of an aerospace vehicle (Aerospace Vehicle Simulation /AVS/ Program simulating continuous and discrete dynamics of aerospace vehicles and ground support equipment on digital computer), 1967-01, p.6P-6P

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2
Typical vehicle parameters for dynamics studies
Typical vehicle parameters for dynamics studies
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Typical vehicle parameters for dynamics studies

R E Rasmussen

S.l. S.N. 1970

Localização: EPBC - Esc. Politécnica-Bib Central    (629.331 R184t f )(Acessar)

3
Fluid and thermodynamic modeling of a nuclear rocket vehicle (Fluid and thermodynamic modeling for ground test simulation of nuclear rocket vehicle liquid hydrogen propellant behavior)
Fluid and thermodynamic modeling of a nuclear rocket vehicle (Fluid and thermodynamic modeling for ground test simulation of nuclear rocket vehicle liquid hydrogen propellant behavior)
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Fluid and thermodynamic modeling of a nuclear rocket vehicle (Fluid and thermodynamic modeling for ground test simulation of nuclear rocket vehicle liquid hydrogen propellant behavior)

Erickson, R C ; Kirkland, F P ; Westerheide, D E

Fluid and thermodynamic modeling of a nuclear rocket vehicle (Fluid and thermodynamic modeling for ground test simulation of nuclear rocket vehicle liquid hydrogen propellant behavior), 1969-01, p.12P-12P

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4
Ground winds and space vehicles (Dynamic excitation by ground winds of large Saturn type launch vehicle structures)
Ground winds and space vehicles (Dynamic excitation by ground winds of large Saturn type launch vehicle structures)
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Ground winds and space vehicles (Dynamic excitation by ground winds of large Saturn type launch vehicle structures)

Reed, T G

ASTRONAUTICS AND AERONAUTICS, 1965-12, Vol.3, p.38-41

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5
Development of a terminal landing rocket system for Apollo-type vehicle (Base-mounted landing rocket system for Apollo- type vehicle evaluated for heat-shield water pressure, ground effect, vehicle dynamics, etc)
Development of a terminal landing rocket system for Apollo-type vehicle (Base-mounted landing rocket system for Apollo- type vehicle evaluated for heat-shield water pressure, ground effect, vehicle dynamics, etc)
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Development of a terminal landing rocket system for Apollo-type vehicle (Base-mounted landing rocket system for Apollo- type vehicle evaluated for heat-shield water pressure, ground effect, vehicle dynamics, etc)

LANDS, J F, J R

AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AERODYNAMIC DECELERATION SYSTEMS CONFERENCE, HOUSTON, TEX.; United States; 7-9 Sept. 1966, 1966, p.196-203

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6
On the use of dynamic models for studying launch vehicle buffet and ground-wind loads (Dynamic models for study of launch vehicle buffeting at transonic speeds and ground-wind loads)
On the use of dynamic models for studying launch vehicle buffet and ground-wind loads (Dynamic models for study of launch vehicle buffeting at transonic speeds and ground-wind loads)
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On the use of dynamic models for studying launch vehicle buffet and ground-wind loads (Dynamic models for study of launch vehicle buffeting at transonic speeds and ground-wind loads)

Hanson, P W ; JONES, G W, J R

AEROSPACE IND. ASSOC. OF AM. PROC. OF SYMP. ON AEROELASTIC AND DYNAMIC MODELING TECHNOL, 1964, p.333-387

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7
Development of a terminal landing rocket system for Apollo-type vehicles (Base-mounted landing rocket system for Apollo type vehicle evaluated for heat-shield water pressure, ground effect, vehicle dynamics, etc)
Development of a terminal landing rocket system for Apollo-type vehicles (Base-mounted landing rocket system for Apollo type vehicle evaluated for heat-shield water pressure, ground effect, vehicle dynamics, etc)
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Development of a terminal landing rocket system for Apollo-type vehicles (Base-mounted landing rocket system for Apollo type vehicle evaluated for heat-shield water pressure, ground effect, vehicle dynamics, etc)

LANDS, J F, J R

JOURNAL OF SPACECRAFT AND ROCKETS, 1967-03, Vol.4, p.333-338

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8
Some research related to the structural dynamics of launch vehicles (Structural dynamics of Saturn I and Saturn V dynamic models - effect of ground wind on launch vehicles)
Some research related to the structural dynamics of launch vehicles (Structural dynamics of Saturn I and Saturn V dynamic models - effect of ground wind on launch vehicles)
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Some research related to the structural dynamics of launch vehicles (Structural dynamics of Saturn I and Saturn V dynamic models - effect of ground wind on launch vehicles)

Runyan, H L

1965 30 P REFS PRESENTED AT THE 6TH INTERN. SYMP. ON SPACE TECHNOL. AND SCI., TOKYO, 29, 1965

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9
Dynamic loads analysis of space vehicle systems - Launch and exit phase (Dynamic loads analysis of space vehicle systems - analytical techniques, ground wind induced loads, engine start and shutdown and launch, atmospheric disturbance, and frequency response)
Dynamic loads analysis of space vehicle systems - Launch and exit phase (Dynamic loads analysis of space vehicle systems - analytical techniques, ground wind induced loads, engine start and shutdown and launch, atmospheric disturbance, and frequency response)
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Dynamic loads analysis of space vehicle systems - Launch and exit phase (Dynamic loads analysis of space vehicle systems - analytical techniques, ground wind induced loads, engine start and shutdown and launch, atmospheric disturbance, and frequency response)

Appleby, B A ; Martin, J D ; Schuett, R H

Dynamic loads analysis of space vehicle systems - Launch and exit phase (Dynamic loads analysis of space vehicle systems - analytical techniques, ground wind induced loads, engine start and shutdown and launch, atmospheric disturbance, and frequency response), 1966, p.246 P-246 P

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10
Dynamics, control and ride quality of a magnetically levitated high speed ground vehicle
Dynamics, control and ride quality of a magnetically levitated high speed ground vehicle
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Dynamics, control and ride quality of a magnetically levitated high speed ground vehicle

Wilkie, Dennis F.

Transportation research, 1972-01, Vol.6 (4), p.343-369

Elsevier B.V

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Deste Autor:

  1. Rasmussen, R

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