RevisedGCOiTIDrTIAljmodel Mercury Capsule

3.10.1.3 RATE STABILIZATION AND CONTROL SYSTEM - A rate stabilization and control system shall be provided. This system, which shall operate independently of the ASCS, shall provide a redundant rate damping feature that shall act as an aerodynamic control response system, providing the astronaut with a control stick steering mode. Movement of the three-axis hand controller shall provide capsule angular rates approximately proportional and corresponding to stick deflection. The rate...

March

3.5' 6 ANTENNA FAIRING - An antenna fairing, in accordance with MAC Drawing No. 45-31003, shall he installed between the cylindrical recovery compartment and the escape tower and shall extend from Sta. Z184.57 to Z208.57. The antenna fairing shall house the pitch and roll horizon scanners. An eight (8) inch window assembly consisting of a silicone base, fiberglass insulation, vycor glass, and teflon strips, shall be located around the outer base of the antenna fairing and shall act as a...

DATtxa MarcxMcdonnell woea

REVISED P Augost i960 S7 LCiilS, MlSSC S REPORT_6603 REVISED 35 AttgWrt i960 mGttW amp mmmt mqph. Mercury Capsule 3.12.5.2.1 ABORT INITIATION - Continued. b. After capsule umbilical separation and prior to missile lift-off 8 inch altitude , an abort can be initiated by radio command and by hard line which by-passes the missile lock-out relay via the missile umbilical. c. After missile lift-off, prior to missile umbilical separation, an abort can be initiated by radio command, by hard line via...

E revised August i Louis Mssoubireport

Revised__fOlVf IT Haiigliiiip'I iifeWi MODR Mercury Capsule 3.3.9.3 ACCELERATION INDICATION - An accelerometer in accordance with MAC Drawing No. 45-61702 shall be provided for the longitudinal axis only. The modified standard accelerometer, in accordance with Specification MIL-A-25719, shall include positive and negative g memory pointers. 3.8.9.4 SEQUENCE SYSTEM AND OVERRIDE CONTROLS - The sequence system shall consist of engraved nameplates and telelight sequence lights with adjacent...

NfnmTWPTTT u

LOUIS, MISSOURI report_6603 hats 12 March 1959 REVISED 5 August I960 REVISED_ 1.1 SCOPE - This specification shall define, the details of design, construction, equipment, testing and data requirements for a Manned Satellite Capsule as follows NASA Designation Project Mercury Designer's Name McDonnell Aircraft Corporation MAC Model Designation Model 133K Number and Places for Crew One Cabin Enclosure Booster Vehicle Atlas D Missile HS-36 1.1.1.1 GENERAL - The mission...

Mopa Mercury Capsule

3.8.8.1.1 RIGHT-HAND CONSOLE - The right-hand console in accordance with MAC Drawing No. 45-81002 shall contain controls for cabin temperature, suit temperature and oxygen supply. These controls shall be accessible to the astronaut while in the fully pressurized condition. The right-hand console shall be finished in light blue space capsule coating XA.-266 compatible with the life support color code as applied to the main instrument panel. 3.8.8.1.2 LEFT-HAND CONSOLE.- The left-hand console in...

A Mcdonnell J

4.2 NASA QUALIFICATION - Capsules supplied by the contractor will he used in a qualification flight test program to he conducted by the NASA. The capsule and its systems shall demonstrate satisfactory performance within the framework of this specification. This qualification program will have as its final objective the accomplishment of the missions described in Paragraph 1.1.1 herein. MAC TESTING - The contractor shall undertake structural, aero dynamic, hydro dynamic, equipment,...

MmnellPAGB

LOUIS, MISSOURI REPORT-6603 date 12 March 1959 U o an, page__J28 revised August I960 ST. LOUIS, MISSOURI report_ 23 SA S-6 revised__mriTFIIWfTT 'IIT model Mercury Capsule GOVERNMENT FURNISHED EQUIBEHT - GOVERNMENT INSTALLED Not Used DATS 12 March 1959 MfflNEU PAGE-'__ revised 5 August I960 sr lquis missour, report_6603. revised__ totf model Mercury Capsule DATS 12 March 1959 MfflNEU PAGE-'__ revised 5 August I960 sr lquis missour, report_6603. revised__ totf model Mercury Capsule...

Mdonnell

3.15.2 TAPE RECORDER - A tape recorder in accordance with MAC Drawing No. 45-88707, shall he provided for permanent data storage. The recorder shall function continuously during all phases of the mission and for 10 minutes after impact for recording of astronaut comments and observations. All voice messages sent to ground stations by the astronaut shall be recorded by this equipment. The tape recorder shall be compatible with the pulse duration modulation system, subcarrier oscillators VCO and...

Am mo Mcdonnell

Mercury Capsule Specification

NinilM m ioiiii un mute ai lt f ti NinilM m ioiiii un mute ai lt f ti IMUII1W U tlM COMI Ot H loairnCMtOMKOil MMC N gt lOtUONUOti SIOTMI revised 5 augl3t i960 st lou s m ss0uri report_6603 msa s6 revised_____aamriDroW l ilP Monw Mercury Capsule WEIGHT AND 3ALANC3 - Specification MIL-W-25l40 and Technical Order 1-1B-40 shall be utilized as reference guides. GROSS WEIGHT - Current weight breakdown and center of gravity of the capsule as described herein is as shown on the following EFFECTIVE...

Revised August is luis missoureport

3.8.9.7 SWITCHES AND HANDLES - Continued All toggle switches except these shall he channel guarded. These shall he positively retained in the normal position hy wire retention clips. DATs 12 March 1959 REVISED 5 August I960 SA S-6 REVISED_ DATs 12 March 1959 REVISED 5 August I960 SA S-6 REVISED_ date 12 March 1959 MCDONNELLCyo dt m page_ revised 5 August i960 ST LOU S MISSOURI report- 93 s'6 revised__rnwitmm.1iiiiv f model Mercury Capsule 3.8.9.8 SWITCH FUSES - Switch fuses shall he provided...