1570nm Laser Rangefinder -120K16
Parameter
| Morbi laoreet | Specification | ||
| Necem | 1570nm | ||
|
Maximum dolor | ≥120km | Vndique de caelo in terram | reflectivity≥0.1 |
| Altitude of aircraft≥6km | |||
| ≥16km | Vndique a terra ad caelum, scopum area: 0.1㎡ | reflectivity≥0.3 | |
| visibility≥16km | |||
| Minimum Range | ≥400m | ||
| Vndique repetitio rate | ≥20Hz | ||
| angulus distinctio | ≤0.6mrad | ||
| accurate vndique | ≤±5m | ||
| Potentia copia | DC 22V~30V | ||
| Virtus (sub locus temperatus) | ≤300W | ||
| Continua operating tempore | ≥3min@20hz | ||
| Operating Temperature | -40℃~+55℃ | ||
| Repono temperatus | -50℃~+65℃ | ||
| Dimension | ≤410mm×231mm×161mm (pilum lens non includitur) | ||
| Pondus | ≤10kg | ||
Cum notis audacibus et perspicuis, speciale consilium nervum et connexiones eam a contrario et falso nexu tueri tendit.Pro instrumento externo, J30J micro-connexiones militares adoptat (nomina variantur secundum artifices diversorum) Socket: XS1
Mensa 1 et mensa 2 nervum et obturaculum instrumenti externi ostendunt, mensa 3 definitionem Pin NO ostendit.
Table 1Socket externa interfacelaser rangefinder
| NO. | Item | Model | Mark |
| 1 | Tabule potestatis copiae et communicationis | J30JM-15ZKP29 | XS1 |
Mensa2 Plugexternae interfacelaser rangefinder
| NO. | Item | Model | Mark |
| 1 | Obturaculum potentiae copiae et communicationis interface | J30J-15TJL-C1(L100) | XP1 |
Tabula 3 Definition of Pin NO.
| ACUS NO. | Abbr. | Nota. | Definition |
| 1 | PWR+ | DC，28V+ |
|
| 2 | PWR+ | DC，28V+ |
|
| 3 | PWR+ | DC，28V+ |
|
| 4 | PWR+ | DC，28V+ |
|
| 5 | RTN_P | DC，28V- |
|
| 6 | RTN_P | DC，28V- |
|
| 7 | RTN_P | DC，28V- |
|
| 8 | RTN_P | DC，28V- |
|
| 9 | LRF_COM_T+ | RS422(COM)Y | Laser rangefinder transmittunt+ |
| 10 | LRF_COM_T- | RS422(COM)Z | Laser rangefinder transmit- |
| 11 | LRF_COM_R- | RS422(COM)B | Laser rangefinder receive- |
| 12 | LRF_COM_R+ | RS422(COM)A | Laser rangefinder accipere+ |
| 13 | GND_ LRF_COM | RS422(COM)GND |
|
| 14 | LRF_ Trigg_R+ | externum felis recipere + |
|
| 15 | LRF_ Trigg _R- | externum felis receive- |
Peltas et conditio necessaria
Facultatem vndique: 120km(vndique de caelo in terram;reflectivity:≥0.1, Altitude aircraft:≥6km)
Vndique facultatem;≥16km (ranging a terra ad caelum, scopo area:0.1㎡, reflectivity:≥0.3, uisibiliter≥16km)
Analysis et verificationis
Praecipui ambitus qui facultatem vndique afficiunt, apicem potentiae lasers sunt;divergence angulus, ttradendi et recipiendi tradendi, necem laseris, etc.
Hoc enim laser rangefinder, capit≥10MWculmen virtutis laserarum, 0 .6mrad d*ivergence angle, 1570um adsum, transmittendi≥XC%, transmissione accepto≥80% et 140mm r *ecipiens aperture.
Laser est repercussor pro parvis scutis, capacitas vndique hac formula computari potest.Vndique formula parva scuta.
Cum 6km altitudine volans et 145km spatio ad scuta, vis minima detectabilis minor quam MDS ipsius APD (5×10-9W) ergo, sub conditione 6km altitudinis volatilis, laser rangefinder eminere potestmagna scuta (de caelo usque ad terram)ad 140 ~ 145km (propinquus vel minus 145km esset).
Cum notis audacibus et perspicuis, speciale consilium nervum et connexiones eam a contrario et falso nexu tueri tendit.Pro instrumento externo, J30J micro-connexiones militares adoptat (nomina variantur secundum artifices diversorum) Socket: XS1
Mensa 1 et mensa 2 nervum et obturaculum instrumenti externi ostendunt, mensa 3 definitionem Pin NO ostendit.
Table 1Socket externa interfacelaser rangefinder
| NO. | Item | Model | Mark |
| 1 | Tabule potestatis copiae et communicationis | J30JM-15ZKP29 | XS1 |
Mensa2 Plugexternae interfacelaser rangefinder
| NO. | Item | Model | Mark |
| 1 | Obturaculum potentiae copiae et communicationis interface | J30J-15TJL-C1(L100) | XP1 |
Tabula 3 Definition of Pin NO.
| ACUS NO. | Abbr. | Nota. | Definition |
| 1 | PWR+ | DC，28V+ |
|
| 2 | PWR+ | DC，28V+ |
|
| 3 | PWR+ | DC，28V+ |
|
| 4 | PWR+ | DC，28V+ |
|
| 5 | RTN_P | DC，28V- |
|
| 6 | RTN_P | DC，28V- |
|
| 7 | RTN_P | DC，28V- |
|
| 8 | RTN_P | DC，28V- |
|
| 9 | LRF_COM_T+ | RS422(COM)Y | Laser rangefinder transmittunt+ |
| 10 | LRF_COM_T- | RS422(COM)Z | Laser rangefinder transmit- |
| 11 | LRF_COM_R- | RS422(COM)B | Laser rangefinder receive- |
| 12 | LRF_COM_R+ | RS422(COM)A | Laser rangefinder accipere+ |
| 13 | GND_ LRF_COM | RS422(COM)GND |
|
| 14 | LRF_ Trigg_R+ | externum felis recipere + |
|
| 15 | LRF_ Trigg _R- | externum felis receive- |
Peltas et conditio necessaria
Facultatem vndique: 120km(vndique de caelo in terram;reflectivity:≥0.1, Altitude aircraft:≥6km)
Vndique facultatem;≥16km (ranging a terra ad caelum, scopo area:0.1㎡, reflectivity:≥0.3, uisibiliter≥16km)
Analysis et verificationis
Praecipui ambitus qui facultatem vndique afficiunt, apicem potentiae lasers sunt;divergence angulus, ttradendi et recipiendi tradendi, necem laseris, etc.
Hoc enim laser rangefinder, capit≥10MWculmen virtutis laserarum, 0 .6mrad d*ivergence angle, 1570um adsum, transmittendi≥XC%, transmissione accepto≥80% et 140mm r *ecipiens aperture.
Laser est repercussor pro parvis scutis, capacitas vndique hac formula computari potest.Vndique formula parva scuta.
Cum 6km altitudine volans et 145km spatio ad scuta, vis minima detectabilis minor quam MDS ipsius APD (5×10-9W) ergo, sub conditione 6km altitudinis volatilis, laser rangefinder eminere potestmagna scuta (de caelo usque ad terram)ad 140 ~ 145km (propinquus vel minus 145km esset).
