Nasa schedules project fire launch news release no. 64-69
Nasa schedule of fire project launchings
FIRE PROJECT↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Project FIRE integrated post flight evaluation report, Flight no. II
Postflight evaluation of FIRE Project second space vehicle
SPACE VEHICLE↗
Flight parameters and vehicle performance for project fire flight 1, launched april 14, 1964
Flight parameters and spacecraft performance for Fire project flight 1
FIRE PROJECT↗
Flow field prediction and analysis, Project Fire
Flow field prediction and analysis - Fire project
FLOW FIELD↗
Project fire integrated post flight evaluation report, flight no. 1
Fire project flight test of Atlas launch vehicle, Antares velocity package, and reentry vehicle
ANTARES MISSILE↗
Project Fire Flight 1 vibration data
Spectral density analysis on Fire Project flight vibration data
FIRE PROJECT↗
Body motion and angles of attack during Project Fire Flight II reentry
Body motion and angles of attack during Fire Project flight reentry
ATMOSPHERIC ENTRY↗
Flow field prediction and analysis, project fire final report
Flow field, and convective and radiative heating predictions for NASA Fire project reentry package trajectories
FLOW FIELD↗
Nasa schedules project fire launch in may
Launching of Project FIRE spacecraft for reentry heating experiments
REENTRY EFFECT↗
Angle-of-attack analysis for Project Fire 1 payload reentry flight
Computer program for Project Fire 1 payload reentry flight angle of attack analysis
ANGLE OF ATTACK↗
Project Fire instrumentation for radiative heating and related measurements
Project Fire instrumentation for radiative heating measurements
FIRE PROJECT↗
Convective and Equilibrium Radiation Heat Transfer Prediction for Project Fire Reentry Vehicle
Convective and equilibrium radiation heat transfer prediction for Project Fire reentry vehicle
FIRE PROJECT↗
Flight parameters and vehicle performance for Project Fire Flight II, launched May 22, 1965
Flight characteristics, and spacecraft performance for Fire Flight II project
FIRE PROJECT↗
Analysis of tethered balloon, ceilometer and class sounding data taken on San Nicolas Island during the FIRE project
During the FIRE Marine Stratocumulus Program on San Nicolas Island, Colorado State University (CSU) and the British Meteorological Office (BMO) operated separate instrument packages on the NASA tethered balloon. The CSU package contained instrumentation for the measurement of temperature, pressure, humidity, cloud droplet concentration, and long and short wave radiation. Eight research flights, performed between July 7 and July 14, are summarized. An analysis priority to the July 7, 8 and 11 flights was assigned for the purposes of comparing the CSU and BMO data. Results are presented. In addition, CSU operated a laser ceilometer for the determination of cloud base, and a CLASS radiosonde site which launched 69 sondes. Data from all of the above systems are being analyzed.
Schubert, Wayne H.↗
STATIC STABILITY INVESTIGATION OF PROPOSED PROJECT FIRE SPACE-VEHICLE AND REENTRY-PACKAGE CONFIGURATIONS AT MACH NUMBERS FROM 1.47 TO 4.63
Project fire - space and reentry vehicle static stability
REENTRY VEHICLE↗
PRESSURE DISTRIBUTIONS OVER THE FORWARD PORTION OF THE PROJECT FIRE SPACE-VEHICLE CONFIGURATION AT MACH NUMBERS FROM 0.25 TO 0.60
Pressure distributions over forward portion of project fire space-vehicle configuration at subsonic speed
PRESSURE DISTRIBUTION↗
SURFACE PRESSURE DISTRIBUTIONS ON 0.0628-SCALE MODELS OF PROPOSED PROJECT FIRE SPACE VEHICLES AT MACH NUMBERS FROM 0.25 TO 4.63
Surface pressure distribution on 0.0628 scale models of proposed project fire space vehicles
PRESSURE DISTRIBUTION↗
Project Fire photographic summary and record of reentry phenomena at hyperbolic velocities
Project Fire was undertaken by the National Aeronautics and Space Administration to measure the total and radiative heating experienced by a blunt body reentering the earth's atmosphere at 11 300 meters per second. This report presents a photographic record of the Fire II spacecraft during its reentry. The photographs were clear enough to establish the times of major events, and they show that adequate-separation was maintained between the reentry package and the spent Antares. This report also identifies operational problems encountered in spacecraft reentry at hyperbolic velocities and presents the solutions satisfactorily employed.
Reentry vehicle↗