A. Noise on Channel 8 Telemetry During Inadvertent Turn-On.

Page

B-5

B-5

B-6

B-7

B-7

B-9

B-9

B-11

C-1

B.

Tests Performed on the Command Switch and on the
15 Point Commutator....

C-4

1.

Test Performed on a 15 Point Commutator to Determine its
Speed Characteristics..

C-4

B. Effect of Diaphragm and Mounting Block Changes on the Measured
Flight Vibration of RA-6 as Compared to RA 1-4.

F-1

1.

Introduction

F-1

G. Search for RCA RF Signals from TV Subsystem During

Boost Phase. . . .

K-8

J

A.

SEQUENCER ACCUMULATOR PULSE AND HIGH CURRENT

REGULATOR CHARACTERISTICS

Operating Characteristics of the Sequencer Accumulator Pulse

L-1

3.

B.

Observations of the Four Frames of Channel 8 Telemetry

Characteristics of the High Current Regulator.

L-1

L-3

4-1

Statistical Distribution of Spacecraft Acceleration Spectra During

Liftoff Based on Five Ranger Flight Measurements

4-3

4-2

4-3

RA-6 Vibration Levels Corrected to RA-1 Through RA-5 During Liftoff..

Statistical Distribution of Spacecraft Acceleration Spectra During

Transonic Flight Based on Five Ranger Flight Measurements

4-4

4-5

4-4

4-5

RA-6 Vibration Levels Corrected to RA-1 Through RA-4 During Transonic.

RA-6 Flight, IRIG Channel 18 .

4-6

4-9

4-9

5-1

RA-6 Measured Flight Vibration Corrected to the Spacecraft Flight .

Analog Record of Channel 8 During Cruise Mode.

4-15

5-2

5-2

Reduced Channel 8 Telemetry Voltages at Prelaunch and During

Inadvertent Turn-On ....

5-10

5-3

5-4

Reduced Channel 8 Telemetry Voltages Following Separation

Reduced Channel 8 Telemetry Voltages During Terminal Phase

5-11

5-12

5-5

RA-6, Full Mission Telemetry Plot, Channel 8, Point 3, F-Battery

Internal Temperature

5-13

5-6

RA-6, Full Mission Telemetry Plot, Channel 8, Point 4, P-Battery

Number

ILLUSTRATIONS (cont)

Title

Page

5-7

RA-6, Mission Telemetry Plot, Channel 8, Point 7, Top Hat,
Temperature, (-Y Axis)

5-15

5-8

RA-6, Mission Plot, Channel 8, Point 8, Shroud Temperature
(-Y Axis)

5-16

7-3

A-1

A-2

RA-6 Agena Separate and Spacecraft Umbilical Connectors.
RA-6. Channel 8, Point 1, Calibration Curve, Unregulated Voltage
RA-6, Channel 8, Point 2 Calibration Curve, Low Current Regulator
Output.

7-6

A-6

A-7

A-3

RA-6, Channel 8, Point 3 Telemetry, Calibration Curve, F Battery
Internal Temperature.

A-8

A-4

RA-6, Channel 8, Point 4, Telemetry Calibration Curve, P Battery
Internal Temperature.

RA-6, Channel 8, Point 7, Telemetry Calibration Curve, Top Hat
Temperature (-Y Axis).

Critical Area of Electrostatic Potential Versus Atmosphere (In Terms
of Altitude and Spark-gap)

E-3

F-1

Channel 17 Power Spectral Density (PSD), 2. 5 to 4. 5 Seconds

F-2

F-2

F-3

Channel 17 Power Spectral Density (PSD), 41. 75 to 43. 75 Seconds.
Channel 17 Power Spectral Density (PSD), 49. 2 to 51. 2 Seconds

F-3

F-4