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_:

3,1957

4,1957

1.4uneh data

Oct.

Nov.

Narno

Z

L[

(U.,_.S.R.)

SPU'rml

_PUrNII[

I

II (no_e

(pay.

I

(case), III

cone).

1957 B_A

I

_I (pay-

1958 E rmx,oN_..

1968 G,u_ ;¢x. ....

(cme); ,oad).

19_8 BZT,:

1968 A_r_t4_._

.......

load),

1957 AL_H£:

International deslgnafAml

CHRONICLE

8int_)

_t_te_)

8int_)

(u.s.s.R.)

EXPIaDnlrB

£

(United

e_t9

FL,ORU'R

(united

Vzwo

81, 1058

17_ 1_8

7on.

Mar.

E x

(Umted

States)

IV

B_'U'FNIX try (u.e.a._.)

E z n..oJutn (Uulml

of Io/_/ee.

_6, 19_8

15, 1068

]_,flr. 26,19fi8

May

July

t t.

OF

Sot

Not

EARTH IAtmch vehicle

weight

Payload

in ocbit:

data

SATELLITES

Total

AND

About

4 tons (unofflclsl). Scientific instrump_tatfon: 184 lbs.

orbit:

10/_7/bW). in

About

2 chemfosl battery transmit-

weight

ters (ceased Total (uno_clal).

emmd

1U10/

prem:rej.

"Laika"

Ccmnlc rays; and X-radla-

Instmmontatlon:

4 tons Scientific, 1,120 Ibe.

test

animal

tion; tamperature;

Experiments: solar ultrsvfolet (dog); Tranmulttera 57.

cuing

_o

rays, temper-

_/11-

5/_/_8

In

lind total (00-tb. _d-

operation

stopped

add

Coemfo

Total weight: 30.8 lbl ........ 8clentlnc instrumentation: 18.13 Ib_ Experiments: mlcrometeorit_, ature& Trm_mltter intermittent 2/28).

rocket bstt_m: indefl-

400

9)

11&87

t (!_3.

107.9

1957-60 Incline,tlon

65°{o

to

Equator.

to

Equator.

_.84"

_.4 e .......

............

' (107. 5) ! Equator,

114.8

103. 7

96.2

Period (minutes)

PROBES, Perigee (st. mL)

SPACE Apogee (st. mL)

142

Oce)

: (217)

_4

140

_88

1,038

1, 57"3 ! (1,171)

2, 458

--i

(_, 459)

121

163

8tatus:

Rexn_rks

earth

Payload

Ist manmade 1141_8 (_2 days).

solar

_tel]lte down

on

Van

in

on

ot

on up

d._

4,rlt/_

r_t-tlon 6/e/e0.

on raft!on 10/_/50.

b_

ALlon

orbfl

inthat

Still

discovered

the rad_ the e._"

important

Down

densities.

Lnfluence

lat biomedical experlme_1 and data disclosed signi_ cent

most

Status: days).

per atmosphero (i_

Made

by

covery of the IGY, atlon belt axotmd identified

_tatos:

(_d belt later Pioneer IIL)

of orbit

_'0/_5/e0.

o]_rvatton_ detarmination

provided

8_abfllty

and

geodetic cluding

,t

pe_r

eerth

estiof 200 to

radiation im-

by Explorer

on

with

in orbit

slightly

the

8 ttn orbit

transmitting

thtped. St#,_: stttl

_ata

lifetime

mated

11OOO_ean. Yielded

Down

data

tempertture. Down _g_,!_ (_3

mierometeo_ta

discovered on

p_t_ and 8_t_:

Provided to

_

belts, etc.

data Mt-, etc. Status: Down

Frovided

Sl_tus:

W.quat_.

to Equator.

110. 27 _0.2_*

106

belt

1,_0

11_.

en _'_'_,

gangm.

L 167

I

I,

opef_

mJere_etoor

tape

7,_ i1_ Mrth'l malmetl¢ et_

,i

rsys

emmd

mlar-pow*ml _

w'lth

tmnpera-

Comic

31 lhe ..... tatlon: 18._

tm_,

m_d

_m-

beacxm en_tte

_t/_,

Te_nnetering emmd

and

Atmo_herk

_,_

About

t_; mJ_-ometeors,

I_.

All

5 con(_umnels

wRh

10/e/_8.

9/3/M). emmd

ehannela oeMed

= Oeigerend S _a-

Total weight: _8.4 lbe. Instrumentation: _8

fields;

!.aectrmUme

prNmlre;

Experiment-:

Immmmmtatlon:

Total weight: ib_ (onomcUd).

and

mcordaf,

Expertment.:

To_Jd weight: lu_name_

ultely.

LI_ other

t mmmulUer

lit

o/bit)

state

_denU_e payload weight: 3.25 lbL

dlsclo_,d..

(TV-

......

d L_losed..

_uptter-C

tnlutrd

......

......

dl_lomd.

Iuplte¢.O

Not

Jupiter-C

count.r_

Erpertn_t-: Mueller countem tlllt_ma

5

2 trm]m_lttor8 current and

t_mamtmlon


" tO

Oct.

Nov.

Dc_

8t_)

Cifl{ONICLE Name

PION EaR I (umted

8taZ_)

Stata_)

IV

UZZD (Unltsd

(UamJd

(Unmd

slam)

8latin

I

g_

_"

l--M_t_

Sta_)

8o_a]_

Ill

PION L'ZB £I (UnJl_l

_oma

DlSCOVmtll

VaNe

(U.S.S.R.)

or "/)r_a_"

Lomw

(Unfed

Pao_.c_

(UaR_t

PIOI_ZZR

of 10/2_e0.

13,19_

_8,1_

17,1960

IS, 1_S

6,19_

8,19_

_t, lg_

Lmme.h date

Dee.

Feb.

Feb.

Apr.

aAs

S_

Suno

......

AND date

earth;

ray

flux,

snd

Pe_4_ce (st. ml.)

PROBES.

l

Y.uc]lm_ tla_

1957-60--Continued Period (mlnutss)

of denelty in space;

(first

extent

of

ionlr.tnE

rad/sUon

bands that tots]

of

field;

osciUat_on

Observation

data higher

tbat

_q

predlo-

departure

magnetic fYom

determlnatio

some

magnetic

measurements

of mlcrometeors first

of interplanetary

Acquired

(_8

vetoe-

after

energy

minutes

rad/aUon

has

and 42.4

atmca-

region

flux before phere _aunch.

sun orbt_

in

IixuZ

04

human

-

rsdh_on

of l_i/_

deep

srom_l

in orbl_Z

m_B_

cycle.

orbit

Down

In in l_-montb

Still

of

8talus:

orbit. 8tatus:DowneerlyMsreh I_.

_

,._/7/_

earth.

2d

24,000-mph

the Down

around 6 mtn.).

Slams:

d_ys).

1 _1_

I

I_

data.

I I_

Iprobe. 8tat_s:

_UOOl_Ul

Status:

list transmittal voice from space.

b_

belt

Ity. Discovered

Attained

reentering

equator/al

field.

Rsd_

Remarks

radiation baud);

a

Is first earth's

hydromagnetlc

flux;

observation

of

altlbsde of 70,700 statute- ............ Determined: mln.

atmosphere

43 hrs. I?_

reentering

P_cmc

before

over South

m_es

Attained

Apo_ce (st. ml.)

SPACE

includretrc-

39 Ibs. in mag-

_._

_

lotoecllptie.

N-6.

on radiation

l data

for 82 In

r_eov-

mllw.

boar_

Yielded

tracked I

of _7,000

space,

[

Status: 0.127 ° to

, to a distance ectlptlc.

o_

4/2_?_0.

in 4/14/_0,

tmp_ted

to cerr_ mizu.k

instrument

mtemts I_ta

decayed

Spltsbm't_u payload

nest

_erable

JF_t ax_

0._o off _.-&

first

of

lO1.46

443 dsy_

s)

125.4

on

9_L 5"7 --8" off

, (u_

of _

.o.4

tione;

of

............

discovery

before

density

of 963

to ign.tte.

of 63,580

PertheUon _om

_! million mike

_46 ,0_0)

176

S'/,_O0 mike

lIMmm

" '_I

............

Internal

s]titude

M stage failed

i Ul eltitude

within

619

from

I.

!

n_les before French

field

Attained

over

.......

magnetic

Radiation e£c.

mstp_etio Moon,

Attained _tmosphere

fnstruAfrica.

•dles ran.

Came _0.

Item

I

reentering

o_

110

Equatorial

pay-

inelud-

Radiation

in paok(12

radla-

in

fields of _t_orle nuelei

and perfo,_neapsul_ Recova_

....

scan-

RadlaUon

venler

84.4 lbl

Payload

weight: lbs.

of

measurements; feld micrometeors; electronic

cosmic and

and _ nm49_tto m_sa; h_v_ _

7o.74 eovor;

iu

_n

to pro-

o_

sps_ kzr

photo-

Radiation

18.40 Ibs ....... in

data ml_Uk.

Aphelion t_ million

Ibs.

8,7.O Ibs.

_vin

lb_

sppanm_

3,24_

_00 Ibs.

(un-

meo_lin_

in orbit

12.95

lnelud_

of Earth

mot_3_ts.

Total b_zm_':

_ts_a_

l_t I_0 IbL

Xx0_tmm_

bad:

rseefvtng

of trsnsm/tt_u,

wright:

pm'tJ_l_; prtmary

Sd m_).

in

_:

Total

dmenod

Cloud _ p_ocem

wul_ht:

I,_00 Ibs ..... _5 !1)8.

for 3 weeks.

Total

Experiment|: m_sm_m_mta _esnnor

eartb.mmm eke_te

of moon.

Ib_

l,eC0 Ibs ....... 244 Ibs. for

v_lnRy

tmJector_,

Total weJ_tht: Yn_tments:

duor tms_

Expurimm_:

tbs. (_dudm_

weight

eosmk

lion of a_n; 0artb 8rod

ma_tor

Expm'Ixmmts: Study g_ components of Int_'phm_tm'y

e_dal). I.us_ents:

Total

days).

8rod

qu

wehtht

Experiments:

mentatlon:

weight

fields

Experlmeuts:

Total weight: 86.4 i_ ........ lmstrumentat|on: 34J lbe..

tsmperaturea;

of

!netlc

spsce

Experiments:

InstrumentaUon:

roomers.

ing 43.7

Total

SATELLITES

L...

I._.

Launch vehicle

rr

.....

IL. ....... Tots]

...........

Tbo_A

gram_

Th_-ZSs_.._

T_

AL

dumo

!Tier-Able

Thor-Able

OF EARTH

........

ALI'Xa.----o.

ram.

......

......

I.nternatlonal des_n

¸None

N_

NG_m

NODe

1_0

O_._.

]9O9 BL..

Non01.

1950

.. ! To'" ws]ght: Instruments: I_

aommunlmtlo_ anee,

dsta

Expurlm_ts: ejected


e.._

,q

Launch date

K

3ta_)

V

States)

CHRONICLE

Ex_oun

AND data

as Dlscove_r

Perlge_ (st. mL)

PROBES,

Apogee (st.mL)

139

136

166

i

e

s)

e ....

° .......

Vnclination

78._

_0e to Equator mock.

,.

1957-60--Continued

130

04

12_,_hrs. 4_.9

Period (minuteS)

3191

Lunar impact on 9/13/S9

_7

480

26,357

SPACE

H ........

Same as Discoverer II ........

Total weight including paddlewbeels:142IbL Experiments: Measure 3 _.tflc levels of earth's radiation belt; TV scanner to relay cloud cover;mtcrometeor detecUon; 2 magnetometer_

Payload

SATELLITES Launch veh/c_

.......

......

_

Weight: 858.4 Ibs. (estimated). Experiments: Measure external and Internal tempers-: tur_; $_udy ma_et/¢ fl_lds of earth and moon; meteoric Particles; heavy nuclei and other pmperttu of cosmic

m_

za_

, (_.

Vansusrd (SLV-_).

[

101. 33

,(_, _)

Total w_ght s_und 100 lb& Instruments: _0 II_. Experiments:emP_/_sl orbit study of _qp_de _skl_, m/emm_4m_It_, X_ns_ and t,mkommm_.

1142

:(101. _)

I

_0

,044)

i

,(671) i

l

' C',s_) { Not diploid..

luno H (19A)..

; :._ 2_ /.::_'..L.L..

Total mdght: 91.15llm........ _zpsdm_ts: _nth-Sun _st tudSst; LrmR_Iplm md Xdmy eoun_, o_m/¢ my _mmt_

Total weight: 614 lbs. _auflf. Ic _telllte; last stage weighin8 3,42_ lbs. without fuel al_ moon on 10/1_/59, plotures _tt_d w_mt into orbit which con. before p_r/gee on 10/18/_. _taim_ 84_ lbe. o_ /mm-u. {-,,-,ta--e totalof/,_ 11_ Psylosd ps._ed 4,$7_ miles _'om the Exp_Immte: Pbotogmpbed bsek e/de of meon.

"Multletage rocket."

Thor-Agena .....

Thor-A_ma

Thor-Able

OF EARTH International designer/on

1959 I)EL_t....

1959 EtE,0__.

......

IO_A. .....

THETA

ETA .......

.........

1959 ZETA--....

Non6

1_

I_

I_

: ..........................

VII

L_wm lII (u.s.8.g.)

[Vawov_zv HI (United States)

LUNt_ IJ (U.8.S.R.)

Dl_covg_R VI (United 8tstes)

(U-q_d

Dl_OVER,t

Aug. 7,10.50EXYLORER ( Uldted

Aug. 13,1959

12,1959

#.t_.19,1959

_p_.

Sept. 18,1959

Oct. 4, 1_

Oct. 13, I_

, Aat of 10/'_,/eo

...................

Remarks

Down

_psuk 9/2S/_

not (47

Acquired valuable dat_ on radiation )eVels, t ransm/_.ted crude cloud cover lm_e, detected ring of ele_r/c_ current circling the es_nh. Status: Position uncertain u of 10/25/60. Reentry covered. Status: days).

Provided comprehe_/ve survey of earth's magnetic field; detailed k_cation of lower edge of mdintion belta; aceurste count of m/erometeodte impact& Status: Still in orbit 10/

Produced photograph of TO percent of moon's tar [fide. Status: Reentered _m'th's atmosphere about 4/20/_0.

as of 8eptaml_r

Provld_l _tg_iflcsnt geopb_lcal data on radlatl_ m_d ma_z_tlc gormz; first penetration of a musor in flight by mi_-omtteorita. Status: "I'racl_n_ beacon inoperative on 12/8/59. As of 6/16/60, information mitted on 3 of 7 expo.,_m_nta not intelligible s_ter 8 months. Data s'cll,I be/rig reee/ved on _ ezlp_ts

--


7,1959

LsLmah d_e

NOV,

1,1_0 81_,el)

I

Sint_)

vebkge

Paylosd

data I

_0

i

104

I perigee I (s¢. =_.)

PROBES.

Apog_ _sZ. =L)

SPACE

Contained telemetry equipment to measure its performanoe.

I

1,000

I

-1o_

233 ,Cm)

429 , (4_) I

120

Tbor-AgeJ_ ....

4_7

479 , (_)

t (ae,O

_g s ('81@

L

_I

|1 o .......

tlon

1957-6{N-Continued Period (minuCze)

96

!

Remarks

but

not

Electrical malfunction prevented stsblUz_tlon in orbit and separation of capsule. Status: Down on 11126/50 (_o days). ejected

103

bu_ not

10/25/_0.

..

_/8/_0 (110

Capsule located. _]tsms: days).

espsub e_

I _]tatu_:

YJaorbit,

funettou_ _ _ty_ hmneb Brutus In orbit 10f_o.

t/tor

_8_ _in pl_l into near ,eJ_nflsr orbit, but re¢own7 opecatio_s m_L_m ctkmed.

jDs_

Status: Inorbit

down

811.d|_ a_" to d_Ysl_ d/p_c.

u'j

!

ii

_'....

//tgMy sucoes_al e¢pbm.. tion of interplanetary space between orbits of Earth and Venus; estabUgbed oommuuicatlon record of 22.5 ndl_on _ on 6/'_/60; made 1st measurements of solar _re effects, l:_rtie.]e ener[tes and distribution, and magnetic field phenomans In interp]ar_etary space. 8_atus: In orbit around

P.._[

90.1 14 ;._,7• to _ (w. _) I] qustor.

_8

I

....

Provided Ist v.lobsl clo_. cover pbotol_r_phs (22,_00 mtaD _om nest c_c_kr orbit. Status: In stable orbit.

--I--[

/

_.? iSS.. 91.1 | _._ AfterStingofmtnm_kets _ May 15, 1960, went into eeeentrle orbit. 191 94. 26 ' (175) '_.@

aso

J

Capsule eontaL_ed telemetry equipment to measure its per[ormcao_

Inter_tlunal dm_z_xku

....

......

Experiments: Htch.euex_ radiation; p_ms, ¢_ndo dillon and solar instruments. counters; ms_tomster; nat. cromet_orlte oount_r; indJcs_or; t_m_

Total wdfht: 270 pounds .... ObjeoUve: Test of expsrl. r_uml TV ¢ecbnic_s¢ bed. tug to worklw_.da metmroloKicsl _yst_m.

ToUd w_lght: 1,700 poo_ ineindluz _d _ em_u_ m_d 300-pound _l_Uk. 0bk_o_ve: Ostlm_ d_ta oa pmFubdon, oommun/cstim_, orbital I:m'formance, stabillsatlon and recovery te_dque¢

Total weight: _ potmd_ ... Obketlve: Det_-m/ms feasibility of nsv/pt.lm_ mteIIlte.

l'ho_Asena....

Total W_tl_t: 10,008 lbl ...... Prmm_ ,-bin: 6,61_ IM,

Total ws_[ht ind_llng ,mr/re M _t_: &000 Ibs. Objective: '/Put of 8_tem for det_rt_3u c_ m Jl/18 humeh. Ln¢l with tn_wed _nsora

OMectlve: Place _bin into orbit _ test li_ mppo_ 8_mns. _ad mbla _ erblt. _ o_ volm mmmamed to greemd _.at_ _ ee_inlmd _dnmmy _ m,m'*

Not dl=el_ed._

1'hot.Able.Star

Thor-Able .....

TboPA b]e IV..

Thor-Age[m ....

1960 Lx_lmx

1#60 Az_e_

1960 BXC¢.. ....

,,eo D-,_ ..... :

__.

lg60 E."_.ON ....

1960Z_,.

Total we_cht: gL8 Ibm., b,-i,.pbe_/o_ "[_er/he_/oa I cludln_ 4 vanes oovered by!_.8 m/Won[_ 1,9 milllonl 4,/_0solar_llslmd_0lb_of, f_)msun, lJ _)msu_.

1959 Ka PJeA......

CHRONICLE OF EARTH SATELLITES AND Now

D_BCOv_KZR VII (United Stste,)

MmA_ II (U_

8Paczcaxn (u.aa.aJ

Dm¢ovzzsut XI (United St.tm)

Ta_mnT I-B (uuited _ta_,)

Tlaos I (United

Plo_,_txa V (Uuited States)

NOV. 20,19S9 DlSCOvza[R VII/ (Uuited states)

Apt.

Apr. _, iteo

94,1_60

Air. IS,I_0

Ms_

A


g

l&l_O

19,1_o

CHRONICLE Namo

Bte_)

Xrl3" States)

TaANSXY U-A (Un/ted States)

D1scovlxll (United

Eczo I (umted

R.)

XIV 8tatm)

II

6_)

(u.s._

e_.,LrT

fffmted

DII_OVE|II

81.£c3g

1_ lOeO Dmcovmsss (Umtsd

lO, 1_o

22,1960

I_tmeh date

rune

Aog.

Aug.

Aug.

_p.

11_llght:

,_nte, _ YV esm_

AND data

I,_0

Ibs.,

_ eta, and _,

Period (minutes) Incllnathm

1957-60--Continued

Perigee (st. mL)

PROBES,

Apogee (st. mL)

(a) 66.7" (b) 65.8°

82081• .....

Rem&r]_

Still active.

1st time 2 active satellites phtved in orbit in single firStatus:

LII_o

tat sueoe_ful r_oovery ma_ mstde object from sl:mm when dAt_ cspsule r_oven_ at sea on 8/11160. Telemetry check poinU increasedby almost400 per cent over previous Dlseov e.XC*A_.

47_ ......

DemoD.stratad use of radk wave reflection for globs oommunlcations, numoro,_ successful transmLssiom visible to naked eye. Status: Affected by aol_ pr_sure, still In orbl 10/_/_0.

Status: Payload minm capsule in orbit 10/25/60.

_.6" .......

1st _ec_ul snsteh of space object 8.(100 feet In atr by 0-119 _, _0 southwest of Ksws/L 8t_os: Payload m/n_s mpeule down 8/15/e0.

_0. 72 64.57 _......

1_ h/olo_e paylo*d recovert, on 18_h orbit ca S/_0/_0, sn_r traveling _,_0 miles. CapSule andes,. r/m" report_Uy landed lea than 7 miles from peed_ term/nod point.

w

80._" ......

_

Cs4_ule ejected and landed In sea muth of Hawafl, glghted hilt not due to rough teas oa 9/15/60. Csnd_ mteUlta down _m 10/]?/eo.

• L5

ll& $ 117, 8

94.1 ,0n.1)

(a) 101.7 (b) 10X.6

180

lgO i

118

945 , (781)

161 n (153)

(a) SS_ tb) 382

436

L,0t9 , (1,199)

211

4"J'J

t.

(a) ee5 (b) _7

SPACE

In-

Satellite weigbt without final stage of rocket: 10,190 I]_C Obj_tlve: Test espeule and eeeovety _ystem _" ultimate dov_opmmt of msanod _rht. ]._xV-'U_nte: _ _-

¢ludin_ _d-stap ess/n_ and _0-1b. etpeule. ObJ_t/_: Gsth_ data _m tm_tmls/_ _ orbital _ tlon and recovt_t to_nlqu_ Alto csmed 104b. trscklns _r_mt ss part of Navy Tnmt/t ntelllte.

Total

Total weight: 132 Ibs ........ ObJeotlve: Plaos 100-1_t Inflatable sphere in orbit.

Total we_ht: 1,700 lbs. Ineluding Sd.stage easing and 300-1b. capsule. Objective: Gather data ou propulsion, eommuni_t/ons, orbital performance, stabfllzs•.ion and reoovery techulques.

Weight of 2 payloads (a) 223 Ibs.; (b) 42 lbs. Objectives: Demoustrate navigation satelltte; Increase accttraey of geodetic measuremerits; provide accurate time standards. Payload: (a) 2 ceetllators infrared scanner, eleet_oul¢ clock and gl, lltetlo nOiSO recelver; (b) Instruments to read eohr mdiation.

Payload

SATELLITES Lsuneh vehicle

Thor Dclt___

Thor-Alack

Th_-A_s....

Not dI._do._d..

_.

Thor-Al_na ....

OF EARTH International designation

Tait:tJ,_ ....

1_0 Etx I t_d IL

!I_0

.....

I_0 IoTa_ .....

IMO Ka.vr_.

.......

1_0 X_UaSD£

I_OMu

Total we/_ht: I,NI0 Ibs., In. dudJ_ 2d-eta_ _ and _0-1b. mp_a]e. Ob_et/w: Goth_ d_ I_ropul_on, eommuulceU_ _bita] performance, atabIH_ and moovery tw.hn/qum /._tmmm_ Inelu_ mmtr_ _ pm'sahuta for recovery, radio beacon and slu.mlnu_ mdsr chaff for reeove_.


f_q

o

t..a tm_

S, lie0

12,1960

l_e0

1,19e0

7,19e0

19,1980

_,

L_unch date

2_'ov.

_Tov.

Nov.

Dee.

Dee.

Dee.

Name

I-B flt_tee)

VHI States)

XVII Bt_tee)

8t_tm)

Bso_

Psyloed

SATELLITES Leunch v_icle

weight:

per minute.

and

capacoded

ionoand pther

in.

on

and

aluminum

119.6

143

117

406

118

501

(st. me)

Perigee

PROBES,

40_Z

_91

1_8

4_t

615

1,423

6,58

Apogee (st. mL)

SPACE

ll_s., includ-

data

AND

_0 equip-

feasJb_ty

Total

Test

!words

fen

me_mre-

90.14 lbs.

weight: Study d/teeS pc_tlve compeMUon;

by of

lbe.

data

easing

1,700

frequency, momen. energy of mk_ome-

tmlmcm.

on and

2d_tage

weight: cspeule. Oath_

teehnique_ lueluded

parachute

optlml

s

f_ablliz£-

communieaUooS,

mtmmeket

performanm,

eSl_Ule,

for _aT.

reentry and beacon

ll_.

chaff

_0

rtd/o

w_dl_t:

md_

Total Provide

Ob}eeUve:

i

lira.,

of global

10,0e0

phot--

weight:

,_-

flight.

sqnip-

M/das

m

of

;and Intrsred cloud cover.

Psyk_d Test

tat

for manned

_-i_rt ers/t. ObJeettvt: ment

To tram _quipsmmt.

Ob}ect/v_:

B ..............................

B.

for recovery,

Uon and recovery Instrumentation

orbital

propulsion,

Objective:

300-]b

eluding

Total

_te

data turn

electron

ment

sphere

Objective:

Total

transmission equipment ble of handllnZ e8,0C0

of active global co_unieaUo0n8 using delayed repeater

Objective:

Tbor-Ab_

rT.......

dbe_asd__

Thet_Alpnm

Ther-Azena

Not

Thor.Delta__.

Thor-Agena

Suno

Star

B..

ing 300 Ibs. of electrical iment.

OF F.ARTH

I ......

Xz .........

MO

International dmtgnatton

1960

toe0

19(}00_waot__.

I_0

neo P_o___.i

1too ]q i.. ....

CHRONICLE

CovkT_n ( Uni*.ed

EXPLORZm (United

II

(United

Du_ovza_

TmOl (United

8pAC_'C_Ale_ rn"

Bt_)

Btatm)

XVI_

(U a.8._)

(United

Dn_ovzazlt

Dt_ovutzjt (United

I

49.9* .......

28.3* .......

Inclin_ tlon

1957-6e--Continued Period

107

I (mmu_) , I

I

112. ?

96. 45

_2

88,6

_2

i l: |.4 ° ....... I

I

[[

Remarks

! [ Tr.qnsmL_iom

is

sucoe_ful]y

and data

'q

re-

ejected

After

func-

analyzed.

ceased

being

achieved

Irecelved and transmitted. [ 8tatu._: Active 10/25/60.

Orbit cefved

capsule

re-

on

recovered ah-craR

be

orbited

se-

cor-

in

bi-

Sputnik burned up re-entry

carrying

as

IHe-

to

object.

midair

achieved.

2d

C-I19 the

_tellRe data with

ground

of • space

by

suceessfulJy

orbits,

orbit

on 1_7/_).

Transmitter UO_

Polar 31 and in air 11/14/e0,

U.S.

covery

14th 19e0.

Satellite related

to

qnired data; esflm_tad time _ months.

8paee_aft

Referred VL

on 12/2/60.

while

surveil-

by

eerrfed

hum_

equipment

ological payload on tmpmgramed

test

3pameraft

contained

lance capsule

_entta

the

48 orblt_

caught

U,S.

achieved;

after

Capsule ah'eraft

t_ue. C-119

orbit

on l_lO_O. Polar

Slst sueomsf_l to date.


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